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	<title>Jet Engine 150-300 &#8211; Minijets</title>
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	<title>Jet Engine 150-300 &#8211; Minijets</title>
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	<item>
		<title>Heinkel HeS 3</title>
		<link>https://minijets.org/en/heinkel-hes-3/</link>
		
		<dc:creator><![CDATA[Philippe Bezard]]></dc:creator>
		<pubdate>Fri, 01 May 2026 12:33:35 +0000</pubdate>
				<category><![CDATA[Jet Engine 150-300]]></category>
		<guid ispermalink="false">https://minijets.org/?page_id=10362</guid>

					<description><![CDATA[<p>Présentation du turboréacteur Heinkel HeS 3 Le Heinkel HeS 3 est l’un des tout premiers turboréacteurs fonctionnels de l’histoire. Conçu à la fin des années 1930 par l’ingénieur allemand Hans von Ohain au sein de la société Heinkel, il est à l’origine du premier vol d’un avion à réaction. Il équipe le prototype Heinkel He [&#8230;]</p>
<p>L’article <a rel="nofollow" href="https://minijets.org/en/heinkel-hes-3/">Heinkel HeS 3</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
]]></description>
										<content:encoded><![CDATA[<h2 class="wp-block-heading"><strong>Presentation</strong> du turboréacteur Heinkel HeS 3</h2>



<p class="wp-block-paragraph">The <strong>Heinkel HeS 3</strong> est l’un des tout premiers turboréacteurs fonctionnels de l’histoire. Conçu à la fin des années 1930 par l’ingénieur allemand <strong>Hans von Ohain</strong> au sein de la société Heinkel, il est à l’origine du premier vol d’un avion à réaction.</p>



<p class="wp-block-paragraph">Il équipe le prototype Heinkel He 178, qui effectue son premier vol le <strong>27 août 1939</strong>, marquant une étape majeure dans l’histoire de l’aviation.</p>



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<h2 class="wp-block-heading"><strong>Conception et architecture</strong></h2>



<p class="wp-block-paragraph">Le HeS 3 est un turboréacteur de conception simple, caractéristique des premières générations :</p>



<ul class="wp-block-list">
<li><strong>Type :</strong> Turbojet (simple flux)</li>



<li><strong>Compresseur :</strong> centrifuge</li>



<li><strong>Chambre de combustion :</strong> annulaire (avec disposition à flux inversé)</li>



<li><strong>Turbine :</strong> mono-étage axiale</li>



<li><strong>Carburant :</strong> kérosène</li>
</ul>



<p class="wp-block-paragraph">Le choix d’un compresseur centrifuge permet une mise au point relativement rapide, au détriment du rendement global.</p>



<hr class="wp-block-separator has-alpha-channel-opacity"/>



<h2 class="wp-block-heading"><strong>Caractéristiques principales</strong> <em>(ordre de grandeur)</em></h2>



<ul class="wp-block-list">
<li><strong>Poussée :</strong> ~ 2,2 kN (≈ 500 lbf, ≈ 225 kgf)</li>



<li><strong>Longueur :</strong> ~ 1,5 m</li>



<li><strong>Diamètre :</strong> ~ 0,9 m</li>



<li><strong>Masse :</strong> ~ 350 à 400 kg</li>
</ul>



<p class="wp-block-paragraph"><em>(Ces valeurs peuvent varier légèrement selon les versions HeS 3A et 3B.)</em></p>



<hr class="wp-block-separator has-alpha-channel-opacity"/>



<h2 class="wp-block-heading"><strong>Développement</strong></h2>



<p class="wp-block-paragraph">Le HeS 3 est issu des premiers travaux de Hans von Ohain sur les turboréacteurs, débutés dès 1935. Il constitue une évolution des prototypes précédents (HeS 1 et HeS 2), encore expérimentaux.</p>



<p class="wp-block-paragraph">Contrairement aux développements britanniques menés par Frank Whittle, ces travaux ont été conduits de manière indépendante en Allemagne.</p>



<hr class="wp-block-separator has-alpha-channel-opacity"/>



<h2 class="wp-block-heading"><strong>Limites et évolution</strong></h2>



<p class="wp-block-paragraph">Malgré son rôle historique, le HeS 3 présente plusieurs limitations :</p>



<ul class="wp-block-list">
<li>Faible taux de compression</li>



<li>Consommation élevée</li>



<li>Potentiel d’évolution limité</li>
</ul>



<p class="wp-block-paragraph">Ces contraintes conduisent rapidement à l’adoption de turboréacteurs à <strong>compresseur axial</strong>, plus performants, comme ceux développés ultérieurement en Allemagne (Jumo 004).</p>



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<h2 class="wp-block-heading"><strong>Héritage</strong></h2>



<p class="wp-block-paragraph">Le HeS 3 reste un moteur fondateur :</p>



<blockquote class="wp-block-quote is-layout-flow wp-block-quote-is-layout-flow">
<p class="wp-block-paragraph">Il est le premier turboréacteur à avoir propulsé un avion lors d’un vol contrôlé, ouvrant la voie à toute l’aviation à réaction moderne.</p>
</blockquote><p>L’article <a rel="nofollow" href="https://minijets.org/en/heinkel-hes-3/">Heinkel HeS 3</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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		<title>Williams FJX-1</title>
		<link>https://minijets.org/en/300-500/william-fjx-1/</link>
		
		<dc:creator><![CDATA[Philippe Bezard]]></dc:creator>
		<pubdate>Thu, 18 Aug 2022 05:38:29 +0000</pubdate>
				<category><![CDATA[Jet Engine 150-300]]></category>
		<guid ispermalink="false">http://tst.minijets.org/?page_id=5948</guid>

					<description><![CDATA[<p>On December 16, 1996, Williams International received a $37.5 million matching grant contract from NASA under its General Aviation Program (GAP). The GAP&#8217;s objective was for Williams to develop a small, ligth weight, ultra quiet, and fuel-efficient turbofan engine for four- to -six passengers, single- and twin-engine general aviation aircraft crusing at 200 knots or [&#8230;]</p>
<p>L’article <a rel="nofollow" href="https://minijets.org/en/300-500/william-fjx-1/">Williams FJX-1</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
]]></description>
										<content:encoded><![CDATA[<div class="wp-block-columns is-layout-flex wp-container-core-columns-is-layout-995f960e wp-block-columns-is-layout-flex">
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<figure class="wp-block-image size-full"><img fetchpriority="high" decoding="async" width="300" height="200" src="http://minijets.org/wp-content/uploads/2022/08/william_fjx-1.jpg" alt="" class="wp-image-5956" srcset="https://minijets.org/wp-content/uploads/2022/08/william_fjx-1.jpg 300w, https://minijets.org/wp-content/uploads/2022/08/william_fjx-1-18x12.jpg 18w" sizes="(max-width: 300px) 100vw, 300px" /><figcaption>Williams FJX-1, du Midland Air Museum (ceux du CMC Leopard II)</figcaption></figure>
</div>



<div class="wp-block-column is-layout-flow wp-block-column-is-layout-flow">
<p class="wp-block-paragraph">On December 16, 1996, Williams International received a $37.5 million matching grant contract from NASA under its General Aviation Program (GAP). The GAP&#8217;s objective was for Williams to develop a small, ligth weight, ultra quiet, and fuel-efficient turbofan engine for four- to -six passengers, single- and twin-engine general aviation aircraft crusing at 200 knots or better.</p>



<p class="wp-block-paragraph">A 550 lb thrust, low-bypass ratio turbofan, designated FJX-1, was developed as an interim power plant.</p>
</div>
</div>



<h2 class="wp-block-heading">Application</h2>


        <div class="wp-block-getwid-custom-post-type custom-post-type-page has-layout-list">
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            <div class="wp-block-getwid-custom-post-type__post-thumbnail">
            <a href="https://minijets.org/en/300-500/william-fjx-1/cmc-leopard-ii/"><img decoding="async" width="500" height="305" src="https://minijets.org/wp-content/uploads/2022/08/CMC_Leopard_2-02.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2022/08/CMC_Leopard_2-02.jpg 500w, https://minijets.org/wp-content/uploads/2022/08/CMC_Leopard_2-02-300x183.jpg 300w, https://minijets.org/wp-content/uploads/2022/08/CMC_Leopard_2-02-18x12.jpg 18w" sizes="(max-width: 500px) 100vw, 500px" /></a>
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        <div class="wp-block-getwid-custom-post-type__post-header">
            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/300-500/william-fjx-1/cmc-leopard-ii/">CMC Leopard II</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>The 001 prototype featured two low-power NPT301 turbojets from Noel Penney Turbines (NPT) Ltd. in Coventry, England. The converted missile engines were intended solely for the 001, and NPT was slated to develop new engines for the final version of the aircraft. But when NPT went bankrupt, the entire Leopard project was delayed for one [&hellip;]</p>
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                    </div><p>L’article <a rel="nofollow" href="https://minijets.org/en/300-500/william-fjx-1/">Williams FJX-1</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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		<title>Continental J402-CA-700</title>
		<link>https://minijets.org/en/150-300/j402/</link>
		
		<dc:creator><![CDATA[Philippe Bezard]]></dc:creator>
		<pubdate>Wed, 27 Jan 2021 10:22:31 +0000</pubdate>
				<category><![CDATA[Jet Engine 150-300]]></category>
		<guid ispermalink="false">http://tst.minijets.org/?page_id=2944</guid>

					<description><![CDATA[<p>The Continental J402-CA-700 is a small short lyfe-cycle turbojet engine developed in the 1970s for missiles and target drones. 20 years after CAE&#8217;s entry into the aircratf gas turbine business with the highly successful J69 engine family, the company began the development of what became its second most important family : the J402 series. In [&#8230;]</p>
<p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/j402/">Continental J402-CA-700</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
]]></description>
										<content:encoded><![CDATA[<p class="wp-block-paragraph">The Continental J402-CA-700 is a small short lyfe-cycle turbojet engine developed in the 1970s for missiles and target drones.</p>



<div class="wp-block-columns is-layout-flex wp-container-core-columns-is-layout-995f960e wp-block-columns-is-layout-flex">
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<figure class="wp-block-image size-large"><img decoding="async" width="800" height="386" src="http://minijets.org/wp-content/uploads/2021/01/CAE_J402-CA-700.jpg" alt="Continental J402-CA-700" class="wp-image-2585" srcset="https://minijets.org/wp-content/uploads/2021/01/CAE_J402-CA-700.jpg 800w, https://minijets.org/wp-content/uploads/2021/01/CAE_J402-CA-700-300x145.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/CAE_J402-CA-700-768x371.jpg 768w, https://minijets.org/wp-content/uploads/2021/01/CAE_J402-CA-700-18x9.jpg 18w" sizes="(max-width: 800px) 100vw, 800px" /><figcaption class="wp-element-caption">Teledyne CAE J402-CA-700. Source : Aviation week, 1982. Teledyne publicity</figcaption></figure>
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<p class="wp-block-paragraph">20 years after CAE&#8217;s entry into the aircratf gas turbine business with the highly successful J69 engine family, the company began the development of what became its second most important family : the J402 series. In 1972, following a competitive evaluation, CAE received a contract from the navy to develop the J402-CA-400 engine to power the McDonnel Douglas Harpoon (AGM-84A), an anti-ship cruise missile.</p>



<p class="wp-block-paragraph">During the early 1970s, the<strong>&nbsp;J402-CA-700</strong>&nbsp;(CAE Model 372-2A)&nbsp;&nbsp;engine was selected to power the&nbsp;<strong>Beech MQM-107 Streaker</strong>&nbsp;Variable-speed Targer Vehicul (VSTT).&nbsp;These target drones were not one-time-use&nbsp;vehicles like the Harpoon missiles were, so the lifetime of the engine had to be extended from 1 hour to 15 hours. To accomplish this, the turbine temperature was reduced, as well as the rotational speeds. A new starter system was included to give the engine the ability to restart. The result was an engine that was slightly less powerful (640&nbsp;lbf vs 660&nbsp;lbf).</p>
</div>
</div>



<h2 class="wp-block-heading">Application</h2>



<div class="wp-block-query is-layout-flow wp-block-query-is-layout-flow"><ul class="wp-block-post-template is-layout-flow wp-block-post-template-is-layout-flow"><li class="wp-block-post post-2949 page type-page status-publish has-post-thumbnail hentry category-plane-150-300">

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<div class="wp-block-column is-layout-flow wp-block-column-is-layout-flow" style="flex-basis:30%"><figure class="wp-block-post-featured-image"><a href="https://minijets.org/en/150-300/j402/bd5j-j402/" target="_self"><img loading="lazy" decoding="async" width="800" height="600" src="https://minijets.org/wp-content/uploads/2024/11/BD5J-J402-Tori-Mac-1.webp" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="BD-5J J402" style="object-fit:cover;" srcset="https://minijets.org/wp-content/uploads/2024/11/BD5J-J402-Tori-Mac-1.webp 800w, https://minijets.org/wp-content/uploads/2024/11/BD5J-J402-Tori-Mac-1-16x12.webp 16w, https://minijets.org/wp-content/uploads/2024/11/BD5J-J402-Tori-Mac-1-300x225.webp 300w, https://minijets.org/wp-content/uploads/2024/11/BD5J-J402-Tori-Mac-1-768x576.webp 768w" sizes="auto, (max-width: 800px) 100vw, 800px" /></a></figure></div>



<div class="wp-block-column is-layout-flow wp-block-column-is-layout-flow" style="flex-basis:70%"><h3 class="wp-block-post-title"><a href="https://minijets.org/en/150-300/j402/bd5j-j402/" target="_self">BD-5J J402</a></h3>

<div class="wp-block-post-excerpt"><p class="wp-block-post-excerpt__excerpt">Le BD-5J de Tori Mac On connait peut de choses sur le BD-5J J402 de Tori Mac, qui se distingue par sa livrée jaune agrémentée de rayures noires et le marquage distinctif “The Trailblazer Project” sur la dérive. Construit avec l’intention d’être équipé d’un turboréacteur Teledyne CAE J402-CA-700 – d’un diamètre équivalent à celui d’un&hellip; </p></div></div>
</div>

</li></ul></div><p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/j402/">Continental J402-CA-700</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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		<title>CAL-Aero jet engine</title>
		<link>https://minijets.org/en/150-300/projet-cal-aero/</link>
		
		<dc:creator><![CDATA[Philippe Bezard]]></dc:creator>
		<pubdate>Wed, 27 Jan 2021 10:17:46 +0000</pubdate>
				<category><![CDATA[Jet Engine 150-300]]></category>
		<guid ispermalink="false">http://tst.minijets.org/?page_id=2940</guid>

					<description><![CDATA[<p>Il&#160;s&#8217;agit un projet de turboréacteur devant équiper un monoplace à&#160; réaction conçu par les professeurs et les étudiants du&#160;Cal-aero&#160;Technical Institute of California en&#160;1949. Un premier prototype, équipé d&#8217;une large chambre à&#160; combustion verticale a été expérimenté. Par contre nous n&#8217;avons aucune information sur le modèle définitif.</p>
<p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/projet-cal-aero/">CAL-Aero jet engine</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
]]></description>
										<content:encoded><![CDATA[<p class="wp-block-paragraph">Il&nbsp;s&#8217;agit un projet de turboréacteur devant équiper un monoplace à&nbsp; réaction conçu par les professeurs et les étudiants du&nbsp;<strong>Cal-aero&nbsp;</strong>Technical Institute of California en&nbsp;<strong>1949</strong>. Un premier prototype, équipé d&#8217;une large chambre à&nbsp; combustion verticale a été expérimenté. Par contre nous n&#8217;avons aucune information sur le modèle définitif.</p>



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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="360" height="372" src="http://minijets.org/wp-content/uploads/2021/01/Calaero-XLC-1-02.jpg" alt="" class="wp-image-2614" srcset="https://minijets.org/wp-content/uploads/2021/01/Calaero-XLC-1-02.jpg 360w, https://minijets.org/wp-content/uploads/2021/01/Calaero-XLC-1-02-290x300.jpg 290w, https://minijets.org/wp-content/uploads/2021/01/Calaero-XLC-1-02-12x12.jpg 12w" sizes="auto, (max-width: 360px) 100vw, 360px" /><figcaption class="wp-element-caption">Premier turboréacteur du Cal-aero à  avoir été expérimenté. Source : photo Interavia février 1949</figcaption></figure>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="360" height="230" src="http://minijets.org/wp-content/uploads/2021/01/Calaero-XLC-1-01.jpg" alt="CAL-Aero turbojet" class="wp-image-2608" srcset="https://minijets.org/wp-content/uploads/2021/01/Calaero-XLC-1-01.jpg 360w, https://minijets.org/wp-content/uploads/2021/01/Calaero-XLC-1-01-300x192.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Calaero-XLC-1-01-18x12.jpg 18w" sizes="auto, (max-width: 360px) 100vw, 360px" /><figcaption class="wp-element-caption">Version destinée à  l&#8217;avion XLC-1. Source : photo Interavia février 1949</figcaption></figure>
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</div><p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/projet-cal-aero/">CAL-Aero jet engine</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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		<title>Turbomeca Marbore I</title>
		<link>https://minijets.org/en/150-300/turbomeca-marbore1/</link>
		
		<dc:creator><![CDATA[Philippe Bezard]]></dc:creator>
		<pubdate>Wed, 27 Jan 2021 10:08:44 +0000</pubdate>
				<category><![CDATA[Jet Engine 150-300]]></category>
		<guid ispermalink="false">http://tst.minijets.org/?page_id=2933</guid>

					<description><![CDATA[<p>Le Turbomeca Marbore I est turboréacteur à compresseur centrifuge, chambre de combustion annulaire, roue d&#8217;injection et turbine axiale à un étage. Il a été développé comme une version plus puissante des Pimene et Palas. Pour éliminer les problèmes rencontrés lors des atterrissages en vol plané du Leduc 010, Le STAé demanda à Turbomeca d&#8217;étudier un [&#8230;]</p>
<p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/turbomeca-marbore1/">Turbomeca Marbore I</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
]]></description>
										<content:encoded><![CDATA[<div class="wp-block-columns is-layout-flex wp-container-core-columns-is-layout-995f960e wp-block-columns-is-layout-flex">
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="500" height="386" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_01.jpg" alt="Turbomeca Marbore I" class="wp-image-2593" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_01.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_01-300x232.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_01-16x12.jpg 16w" sizes="auto, (max-width: 500px) 100vw, 500px" /><figcaption class="wp-element-caption">Turbomeca Marbore I, N°23 en essai chez Continental aux États-Unis</figcaption></figure>
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<p class="wp-block-paragraph">Le Turbomeca Marbore I est turboréacteur à compresseur centrifuge, chambre de combustion annulaire, roue d&#8217;injection et turbine axiale à un étage. Il a été développé comme une version plus puissante des Pimene et Palas.</p>



<p class="wp-block-paragraph">Pour éliminer les problèmes rencontrés lors des atterrissages en vol plané du Leduc 010, Le STAé demanda à Turbomeca d&#8217;étudier un turboréacteur de 300 kg de poussée. En plaçant un exemplaire à chaque extrémité des ailes, il permettrait à ce dernier de manœuvrer pour atterrir normalement.</p>



<p class="wp-block-paragraph">Ce moteur fut baptisé <strong>Marboré I</strong>. Après des essais au banc en i en avril 1950, il effectue son premier vol le <strong>16 juin 1951</strong> sur le <a href="https://minijets.org/en/150-300/turbomeca-marbore1/cm88-mrk2/" data-type="page" data-id="2963">Fouga Gémeaux</a> (dans sa version CM88 Mrk II). Il volera avec le <a href="https://fr.wikipedia.org/wiki/Leduc_(avion)" data-type="URL" data-id="https://fr.wikipedia.org/wiki/Leduc_(avion)" target="_blank" rel="noopener">Leduc 016</a>  le <strong>15 janvier 1952</strong>.</p>



<figure class="wp-block-image size-full"><img loading="lazy" decoding="async" width="700" height="385" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_05.jpg" alt="Turbomeca Marbore I" class="wp-image-2594" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_05.jpg 700w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_05-300x165.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_05-18x10.jpg 18w" sizes="auto, (max-width: 700px) 100vw, 700px" /><figcaption class="wp-element-caption">Turboméca Marboré I. Source : Flight, 29 june 1951</figcaption></figure>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="500" height="694" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_09.jpg" alt="" class="wp-image-2595" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_09.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_09-216x300.jpg 216w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_09-9x12.jpg 9w" sizes="auto, (max-width: 500px) 100vw, 500px" /><figcaption class="wp-element-caption">Turbomeca Marbore I, Poussée et consommation au point fixe. Source : Fiche documentaire Turbomeca N°02-03, mai 1951</figcaption></figure>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="500" height="694" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_08.jpg" alt="" class="wp-image-2587" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_08.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_08-216x300.jpg 216w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_08-9x12.jpg 9w" sizes="auto, (max-width: 500px) 100vw, 500px" /><figcaption class="wp-element-caption">Turbomeca Marbore I, Courbe de consommation et puissance. Source : Fiche documentaire Turbomeca N°02-03, mai 1951</figcaption></figure>
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<figure class="wp-block-image size-large is-resized"><img loading="lazy" decoding="async" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_06.jpg" alt="" class="wp-image-2591" width="850" height="342" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_06.jpg 850w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_06-300x121.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_06-768x309.jpg 768w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Marbore_I_06-18x7.jpg 18w" sizes="auto, (max-width: 850px) 100vw, 850px" /><figcaption class="wp-element-caption">Encombrement du Turbomeca Marbore I. Source : Fiche documentaire Turbomeca N°02-03, mai 1951</figcaption></figure>



<h2 class="wp-block-heading">Application</h2>


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            <a href="https://minijets.org/en/150-300/turbomeca-marbore1/cm88-mrk2/"><img loading="lazy" decoding="async" width="350" height="256" src="https://minijets.org/wp-content/uploads/2021/01/Fouga_Gemeaux_II.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Fouga_Gemeaux_II.jpg 350w, https://minijets.org/wp-content/uploads/2021/01/Fouga_Gemeaux_II-300x219.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Fouga_Gemeaux_II-16x12.jpg 16w" sizes="auto, (max-width: 350px) 100vw, 350px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-marbore1/cm88-mrk2/">Fouga CM88R Gémeaux mark II</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>L&#8217;exemplaire N° 2 du Fouga&nbsp;CM88R Gémeaux mark II a fait son premier vol aux mains de&nbsp;Léon Bourrieau&nbsp;le&nbsp;16 juin 1951. L&#8217;avion était immatriculé&nbsp;F-WFKN. Sur le plan central entre les deux fuselages se trouvait l&#8217;un dès premiers exemplaires du réacteur&nbsp;Marboré I&nbsp;de Turbomeca. Ce moteur donnait une poussée maximale d&#8217;environ&nbsp;275 à&nbsp; 300&nbsp;Kg pour un poids d&#8217;environ 120 kg. [&hellip;]</p>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="350" height="256" src="http://minijets.org/wp-content/uploads/2021/01/Leduc_016.jpg" alt="" class="wp-image-2596" srcset="https://minijets.org/wp-content/uploads/2021/01/Leduc_016.jpg 350w, https://minijets.org/wp-content/uploads/2021/01/Leduc_016-300x219.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Leduc_016-16x12.jpg 16w" sizes="auto, (max-width: 350px) 100vw, 350px" /><figcaption class="wp-element-caption">The Leduc 016 was developed with wingtip mounted Marbore I</figcaption></figure>
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</div><p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/turbomeca-marbore1/">Turbomeca Marbore I</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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		<title>Turbomeca Aspin I</title>
		<link>https://minijets.org/en/150-300/turbomeca-aspin1/</link>
		
		<dc:creator><![CDATA[Philippe Bezard]]></dc:creator>
		<pubdate>Wed, 27 Jan 2021 09:56:01 +0000</pubdate>
				<category><![CDATA[Jet Engine 150-300]]></category>
		<guid ispermalink="false">http://tst.minijets.org/?page_id=2923</guid>

					<description><![CDATA[<p>The Turbomeca Aspin I is a turbojet with ducted fan, single stage compressor and two stage turbine. Air intake and fan Annular air entry containing one row of variable-incidence entry vanes, a single stage compressor fan and one row of fixed straightening vanes. Fan is driven by compressor shaft through coupling and reduction gear. After [&#8230;]</p>
<p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/turbomeca-aspin1/">Turbomeca Aspin I</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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<figure class="wp-block-image size-full"><img loading="lazy" decoding="async" width="500" height="331" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Aspin_I_01.jpg" alt="" class="wp-image-2606" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Aspin_I_01.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Aspin_I_01-300x199.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Aspin_I_01-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /><figcaption class="wp-element-caption">Turboméca Aspin I. Source : Magazine Flight, février 1951</figcaption></figure>
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<p class="wp-block-paragraph">The Turbomeca Aspin I is a turbojet with ducted fan, single stage compressor and two stage turbine.</p>



<h3 class="wp-block-heading">Air intake and fan</h3>



<p class="wp-block-paragraph">Annular air entry containing one row of variable-incidence entry vanes, a single stage compressor fan and one row of fixed straightening vanes.</p>



<p class="wp-block-paragraph">Fan is driven by compressor shaft through coupling and reduction gear. After fan the air is divided into primary and secondary flows, the former passing to the power section and the latter by-passing that section in an annular casing to the tailpipe where it mixes with the primary jet efflux.</p>



<h3 class="wp-block-heading">Compressor</h3>



<p class="wp-block-paragraph">Single-stage centrifugal compressor. Single-sided impeller.</p>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="500" height="200" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Aspin_I_02.jpg" alt="" class="wp-image-2605" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Aspin_I_02.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Aspin_I_02-300x120.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Aspin_I_02-18x7.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /><figcaption class="wp-element-caption">Turboméca Aspin I. Source : Turbojet History and development, vol. 2</figcaption></figure>
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<h3 class="wp-block-heading">Combustion chamber</h3>



<p class="wp-block-paragraph">Annular type, with rotary fuel injection as in Piméné</p>



<h3 class="wp-block-heading">Turbin</h3>



<p class="wp-block-paragraph">Two-stage axial flow turbine</p>



<h3 class="wp-block-heading">Jet Pipe</h3>



<p class="wp-block-paragraph">Fixed inner cone, annular turbine nozzle and outer pipe wherein the jet efflux and by passed secondary air mix.</p>
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<h3 class="wp-block-heading">Control</h3>



<p class="wp-block-paragraph">Single throttle lever determine the fuel flow and position of variable incidence vanes. Egine speed controled by centrifugal governor. For rapid manoeuvrability a push button operates and electro-hydraulic servo-motor with over-rides manual control and at maximum rotation speed the throttle lever can be used solely to control the entry vanes to obtain rapid variation of thrust without having to oercome the inertia of the rotating assembly.</p>



<h3 class="wp-block-heading">Starting</h3>



<p class="wp-block-paragraph">Throttle at &#8220;starter&#8221; setting only controls fuel delivery. Entry vanes are closed and engine speed governor is ineffective. Normal starter spins rotating assembly. When engine reaches a rotating speed of 70 per cent. of maximum governor and vane become operative.</p>



<h2 class="wp-block-heading">Application</h2>



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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="500" height="333" src="http://minijets.org/wp-content/uploads/2021/01/Fouga_gemeaux_IV_-_0119172158.jpg" alt="" class="wp-image-2607" srcset="https://minijets.org/wp-content/uploads/2021/01/Fouga_gemeaux_IV_-_0119172158.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Fouga_gemeaux_IV_-_0119172158-300x200.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Fouga_gemeaux_IV_-_0119172158-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /><figcaption class="wp-element-caption">Fouga CM.88 Gemeaux Mk. IV</figcaption></figure>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="500" height="333" src="http://minijets.org/wp-content/uploads/2021/01/Dorand_01.jpg" alt="" class="wp-image-2603" srcset="https://minijets.org/wp-content/uploads/2021/01/Dorand_01.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Dorand_01-300x200.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Dorand_01-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /><figcaption class="wp-element-caption">Dorand DH-11</figcaption></figure>
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</div><p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/turbomeca-aspin1/">Turbomeca Aspin I</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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		<title>Turbomeca Palas</title>
		<link>https://minijets.org/en/150-300/turbomeca-palas/</link>
		
		<dc:creator><![CDATA[Philippe Bezard]]></dc:creator>
		<pubdate>Tue, 26 Jan 2021 17:07:34 +0000</pubdate>
				<category><![CDATA[Jet Engine 150-300]]></category>
		<guid ispermalink="false">http://tst.minijets.org/?page_id=2891</guid>

					<description><![CDATA[<p>Le Turbomeca Palas, est un réacteur à simple flux, doté d&#8217;un compresseur centrifuge et d&#8217;une turbine axiale, dont les essais commencèrent en septembre 1950. Il sera utilisé pour propulser des avions légers, des planeurs, comme réacteur d&#8217;appoint sur moyen porteur; ainsi que sur un hydroglisseur Au moins deux versions ont été mise sur le marché [&#8230;]</p>
<p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/turbomeca-palas/">Turbomeca Palas</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="600" height="311" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_08.jpg" alt="Turboréacteur Turbomeca Palas" class="wp-image-2912" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_08.jpg 600w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_08-300x156.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_08-18x9.jpg 18w" sizes="auto, (max-width: 600px) 100vw, 600px" /><figcaption class="wp-element-caption">Turbomeca Palas. Source : Brochure Turbomeca</figcaption></figure>
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<p class="wp-block-paragraph">The <strong><a href="#turbomeca">Turbomeca</a> Palas</strong>, est un réacteur à simple flux, doté d&#8217;un compresseur centrifuge et d&#8217;une turbine axiale, dont les essais commencèrent en <strong>septembre 1950</strong>. Il sera utilisé pour propulser des avions légers, des planeurs, comme réacteur d&#8217;appoint sur moyen porteur; ainsi que sur un hydroglisseur</p>



<p class="wp-block-paragraph">Au moins deux versions ont été mise sur le marché :</p>



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<li>Le PALAS I&nbsp;délivrant 150 kgp</li>



<li>Le PALAS II&nbsp;délivrant 160 kgp.</li>
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<p class="wp-block-paragraph"></p>
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<h3 class="wp-block-heading">Compressor</h3>



<p class="wp-block-paragraph">Il s&#8217;agit d&#8217;un compresseur centrifuge à un étage et à 16 pales, en aluminium.</p>



<h3 class="wp-block-heading">Chambre&nbsp;à combustion</h3>



<p class="wp-block-paragraph">La chambre de combustion est de type annulaire avec une distribution du carburant s&#8217;effectuant par l&#8217;intermédiaire d&#8217;une roue à injection. Cette roue est portée par l&#8217;axe de turbine sur lequel est lui-même fixé le compresseur. A sa périphérie elle est percée d&#8217;un certain nombre de conduit par lesquels circule le carburant. Lorsque du carburant est introduit dans l&#8217;intérieur de la roue, il est évacué et pulvérisé&nbsp;dans la chambre à combustion par la force centrifuge. Le débit du carburant est réglé par un clapet de dérivation.</p>



<h3 class="wp-block-heading">Turbin</h3>



<p class="wp-block-paragraph">La turbine est à un étage avec 24 (ou 25) pales. Elle est précédée par un stator équipé d&#8217;une vingtaine d&#8217;entrée. La température max est de 700 °C avant turbine, et de 600 après.</p>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="323" height="590" src="http://minijets.org/wp-content/uploads/2021/01/palas-01t.jpg" alt="Turboréacteur Turbomeca Palas" class="wp-image-2872" srcset="https://minijets.org/wp-content/uploads/2021/01/palas-01t.jpg 323w, https://minijets.org/wp-content/uploads/2021/01/palas-01t-164x300.jpg 164w, https://minijets.org/wp-content/uploads/2021/01/palas-01t-7x12.jpg 7w" sizes="auto, (max-width: 323px) 100vw, 323px" /><figcaption class="wp-element-caption">Turbomeca Palas N°136. Source : Collection philippe Bezard</figcaption></figure>
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<h3 class="wp-block-heading">Pompe à carburant</h3>



<p class="wp-block-paragraph">Pompe Turbomeca, avec une pression maximum 4 kg./cm²</p>



<h3 class="wp-block-heading">Carburant et huile</h3>



<p class="wp-block-paragraph">Kerosene (Jet A1).<br>Air 3512</p>



<h3 class="wp-block-heading">Démarrage</h3>



<p class="wp-block-paragraph">Pour le démarrage, il peut être équipé d&#8217;un démarreur électrique Air Equipement&nbsp; (24 volt) ou d&#8217;une rampe de démarrage à air comprimée.&nbsp;</p>



<p class="wp-block-paragraph">L&#8217;allumage se fait par l&#8217;intermédiaire de 2 bougies qui dans les dernières versions étaient équipées d&#8217;un dispositif d&#8217;injection permettant de démarrer directement sur Kérosène.</p>



<h3 class="wp-block-heading">Mounting</h3>



<p class="wp-block-paragraph">Trois points d&#8217;ancrage, 2 au-dessus du compresseur, un en arrière de la chambre&nbsp;à combustion.</p>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="500" height="318" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_04.jpg" alt="Réacteur Turbomeca Palas fabriqué par Black Burn" class="wp-image-2867" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_04.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_04-300x191.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_04-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /><figcaption class="wp-element-caption">Palas construit sous licence par BlackBurn sous la dénomination Palas 600. Source : Black Burn &amp; General Aircraft LTD., collection Philippe Bezard</figcaption></figure>



<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="597" height="344" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_02.jpg" alt="Dimensions du réacteur Turbomeca Palas" class="wp-image-2879" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_02.jpg 597w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_02-300x173.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_02-18x10.jpg 18w" sizes="auto, (max-width: 597px) 100vw, 597px" /></figure>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="500" height="393" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_05.jpg" alt="Ensemble Turbine et roue d'injection du réacteur Turbomeca Palas" class="wp-image-2870" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_05.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_05-300x236.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_05-15x12.jpg 15w" sizes="auto, (max-width: 500px) 100vw, 500px" /><figcaption class="wp-element-caption">Turbine du Turbomeca Palas. Source : Philippe Bezard</figcaption></figure>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="500" height="284" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_06.jpg" alt="Eclaté du réacteur Turbomeca Palas" class="wp-image-2881" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_06.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_06-300x170.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_06-18x10.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></figure>
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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="1000" height="222" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_03.jpg" alt="Compresseur réacteur Turbomeca Palas" class="wp-image-2871" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_03.jpg 1000w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_03-300x67.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_03-768x170.jpg 768w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_03-18x4.jpg 18w" sizes="auto, (max-width: 1000px) 100vw, 1000px" /><figcaption class="wp-element-caption">Turbomeca Palas, le compresseur centrifuge. Collection Philippe Bezard</figcaption></figure>



<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="1000" height="316" src="http://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_01.jpg" alt="Vue du réacteur Turbomeca Palas" class="wp-image-2868" srcset="https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_01.jpg 1000w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_01-300x95.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_01-768x243.jpg 768w, https://minijets.org/wp-content/uploads/2021/01/Turbomeca_Palas_-_01-18x6.jpg 18w" sizes="auto, (max-width: 1000px) 100vw, 1000px" /></figure>



<h2 class="wp-block-heading">Application</h2>


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            <a href="https://minijets.org/en/150-300/turbomeca-palas/caproni-trento-f5/"><img loading="lazy" decoding="async" width="500" height="299" src="https://minijets.org/wp-content/uploads/2021/01/Caproni_F5_09.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Caproni_F5_09.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Caproni_F5_09-300x179.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Caproni_F5_09-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/caproni-trento-f5/">Aero Caproni Trento F5</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>L&#8217;Aero Caproni Trento F5 a été conçu par Stelio Frati. C&#8217;est le second avion à réaction produit en Italie après le Fiat G-80 (ce dernier étant, il est vrai, beaucoup plus puissant). La période d&#8217;après guerre n&#8217;a pas été facile pour la vieille firme italienne CAPRONI. Elle a eu d&#8217;énormes difficultés et on a annoncé [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/am12-palas/"><img loading="lazy" decoding="async" width="500" height="358" src="https://minijets.org/wp-content/uploads/2021/01/Mantelli_AM12_Palas_01.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Mantelli_AM12_Palas_01.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Mantelli_AM12_Palas_01-300x215.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Mantelli_AM12_Palas_01-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/am12-palas/">AM-12 &#8211; Palas</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>L&#8217;AM-12 &#8211; Palas est un motoplaneur à réaction, étudié par Adriano Mantelli au début des années 60. Même si ses origines rappellent l&#8217;AM-10, l&#8217;AM-12 n&#8217;est pas un Alaparma. Seules les initiales de leur concepteur, Adriano MANTELLI, permettent de trouver une filiation entre ces deux machines. A l&#8217;origine, l&#8217;AM-12 était un planeur. Il a été par la [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/bd-5j-palas/"><img loading="lazy" decoding="async" width="500" height="327" src="https://minijets.org/wp-content/uploads/2021/01/BD-5J_Palas_-_02.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/BD-5J_Palas_-_02.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/BD-5J_Palas_-_02-300x196.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/BD-5J_Palas_-_02-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/bd-5j-palas/">BD-5J Palas</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>BD-5J équippé d&#8217;un Palas par Gary Lyon Le BD-5j Palas est une construction originale, conçue et construite par Gary Lyon (Tennesse). Elle utilise une cellule de BD-5B avec l&#8217;aile de 20 ft et non celle de 17, et est équipée d&#8217;un réacteur Turbomeca Palas. Le réacteur est le N°97 qui équipait auparavant le Sipa 200 [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/cvv6-canguro-palas/"><img loading="lazy" decoding="async" width="500" height="347" src="https://minijets.org/wp-content/uploads/2021/01/CVV6_-_canguro_palas_-_09.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/CVV6_-_canguro_palas_-_09.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/CVV6_-_canguro_palas_-_09-300x208.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/CVV6_-_canguro_palas_-_09-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/cvv6-canguro-palas/">CVV6 Canguro Palas</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>A l&#8217;origine du CVV6 Canguro Palas, Le Canguro est un planeur en bois, biplace, à aile haute, et d&#8217;environ 20m d&#8217;envergure. Il a été conçu en 1939 par le centre de vol à&nbsp;voile de l&#8217;institut Polytechnique de Milan (Centro Volo a Vela del Politecnico Di Milano) sous la direction de l&#8217;Ingénieur&nbsp;Ermenegildo Preti. En plus du [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/fouga-cm-8-r-83-midget/"><img loading="lazy" decoding="async" width="500" height="290" src="https://minijets.org/wp-content/uploads/2021/01/Fouga_Midget_-_05.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Fouga_Midget_-_05.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Fouga_Midget_-_05-300x174.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Fouga_Midget_-_05-18x10.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/fouga-cm-8-r-83-midget/">Fouga CM8 R8.3 Midget</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Le Fouga CM8 R8.3 Midget, avion de course, est le fruit de l&#8217;adaptation du Fouga Cyclope II à la compétition aérienne. À la fin de l’année 1951, la société des « Courses Aériennes », dirigée par le colonel Dohme, passa commande de huit exemplaires auprès des usines Fouga. Ces dernières lancèrent leur production dès novembre [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/fouga-cm8-r98-cyclope-ii/"><img loading="lazy" decoding="async" width="500" height="312" src="https://minijets.org/wp-content/uploads/2021/01/Fouga_cyclope_II-_04.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Fouga_cyclope_II-_04.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Fouga_cyclope_II-_04-300x187.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Fouga_cyclope_II-_04-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/fouga-cm8-r98-cyclope-ii/">Fouga CM8 R9.8 Cyclope II</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Le Fouga CM8 R9.8 Cyclope II, est une évolution de la version Cyclope I qui a été renforcée afin, d&#8217;accueillir un réacteur Turbomeca Palas de 160 Kp en lieu et place de la dernière évolution du Piméné de 110 Kp. Un seul exemplaire a été construit. il a été immatriculé&nbsp;F-WFKM. Positionné sur le marché du [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/ikarus-451m/"><img loading="lazy" decoding="async" width="500" height="333" src="https://minijets.org/wp-content/uploads/2021/01/Icarus_451M_01.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Icarus_451M_01.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Icarus_451M_01-300x200.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Icarus_451M_01-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/ikarus-451m/">Ikarus 451M</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Le capitaine&nbsp;Tugomir Prebeg&nbsp;a effectué le premier vol de cet appareil, premier avion à &nbsp;réaction yougoslave, dans la matinée du&nbsp;25 octobre 1952. L&#8217;Ikarus 451M était un avion expérimental, tout métallique, conçu par le&nbsp;major Dragoljub Beslin, construit par la compagnie IKARUS et propulsé par 2 turboréacteurs Turbomeca Palas. Un seul exemplaire a été construit. Il a servi comme [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/ikarus-452-m/"><img loading="lazy" decoding="async" width="500" height="300" src="https://minijets.org/wp-content/uploads/2021/01/Ikarus_452_01.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Ikarus_452_01.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Ikarus_452_01-300x180.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Ikarus_452_01-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/ikarus-452-m/">Ikarus 452M</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Ikarus L&#8217;Ikarus 452M est un avion expérimental à réaction construit en 1953 en Yougoslavie par l&#8217;équipe de  Dragoljub Beslin. Après la deuxième guerre mondiale, l&#8217;industrie aéronautique yougoslave s&#8217;est réorganisée autour d&#8217;un établissement central chargé des recherches et des réalisations de prototypes, auxquels seront rattachés quelques usines de moindre importance. Cet établissement central perpétue le nom [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/ikarus-s451-m-zolja/"><img loading="lazy" decoding="async" width="500" height="329" src="https://minijets.org/wp-content/uploads/2021/01/Ikarus_S451M_zolja_03.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Ikarus_S451M_zolja_03.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Ikarus_S451M_zolja_03-300x197.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Ikarus_S451M_zolja_03-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/ikarus-s451-m-zolja/">Ikarus S451M Zolja</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Ikarus L&#8217;IKARUS S451M Zolja (Guèpe) n&#8217;est pas à vraiment parler une extrapolation du premier de l&#8217;Ikarus 451M. C&#8217;est un appareil nouveau, monoplace bi-réacteurs. Il a été développé par Dragoljub Beshlin, et a fait son premier vol en 1954. Ayant été conçu comme avion d&#8217;entrainement et comme avion d&#8217;attaque léger, Il est d&#8217;une structure entièrement métallique.&nbsp;Il était prévu pour entrer [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/miles-m77-sparrowjet/"><img loading="lazy" decoding="async" width="500" height="333" src="https://minijets.org/wp-content/uploads/2021/01/Miles_M77_SparrowJet-08.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Miles_M77_SparrowJet-08.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Miles_M77_SparrowJet-08-300x200.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Miles_M77_SparrowJet-08-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/miles-m77-sparrowjet/">Miles M77 Sparrowjet</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Dès sa création, en 1948, la&nbsp;nouvelle entreprise&nbsp;F.G.Miles Ltd.&nbsp; s&#8217;est orientée vers la production d&#8217;avions légers en petite série. Parmi ceux-ci, on retrouve la transformation d&#8217;un avion d&#8217;avant guerre (1936), le&nbsp;Miles&nbsp;M-5 Sparrowhawk&nbsp;&nbsp;G-ADNL en racer à réaction, sous la dénomination&nbsp;Miles&nbsp;M77 SparrowJet. Une résurrection La construction du SparrowJet est sans doute l&#8217;un dès plus bel exemple de résurrection [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/payen-pa-49/"><img loading="lazy" decoding="async" width="500" height="332" src="https://minijets.org/wp-content/uploads/2021/01/Payen_PA49_Katy_08.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Payen_PA49_Katy_08.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Payen_PA49_Katy_08-300x199.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Payen_PA49_Katy_08-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/payen-pa-49/">Payen PA-49 Katy</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Le Payen PA-49 Katy est l&#8217;œuvre de Nicolas-Roland PAYEN, ingénieur d&#8217;avant-garde, père de l&#8217;aile delta.  C&#8217;est un monoplan sans empennage à aile surbaissée. Il est équipé d&#8217;un Turbomeca PALAS et d&#8217;un atterrisseur tricycle fixe. Performances En mai 1951, M.Payen et trois ouvriers construisent le PA-49A en un mois. Il faudra attendre la fin 1952 et tout un grand nombre de [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/short-sb4-sherpa/"><img loading="lazy" decoding="async" width="500" height="337" src="https://minijets.org/wp-content/uploads/2021/01/Short_SB4_04.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Short_SB4_04.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Short_SB4_04-300x202.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Short_SB4_04-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/short-sb4-sherpa/">Short SB-4 Sherpa</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Le premier vol du short SB-4 Sherpa a été effectué à&nbsp;Belfast&nbsp;le&nbsp;4 octobre 1953&nbsp;à &nbsp;partir de l&#8217;aérodrome de Sydenham près de BELFAST, aux mains de&nbsp;Tom Brooke-Smith, chef pilote de Short Brothers, qui a été enchanté, parait-il, des réactions de l&#8217;avion. Il s&#8217;agissait d&#8217;un avion expérimental, destiné à étudier les particularités d&#8217;une aile de type aero-isoclinic. La [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/sipa-300/"><img loading="lazy" decoding="async" width="500" height="333" src="https://minijets.org/wp-content/uploads/2021/01/Sipa_300_-_11.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Sipa_300_-_11.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/Sipa_300_-_11-300x200.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Sipa_300_-_11-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/sipa-300/">Sipa 300</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Le SIPA 300, conçu par Yves Gardan et le bureau d&#8217;études de la SIPA, est un avion d&#8217;entraînement à réaction de premier niveau. Ce biplace en tandem, doté d&#8217;une aile basse et d&#8217;un empennage cruciforme, a effectué son premier vol piloté par Max Fischl le 4 octobre 1954. Historique Entre 1953 et 1954,sous la direction [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/sipa-200-minijet/"><img loading="lazy" decoding="async" width="500" height="318" src="https://minijets.org/wp-content/uploads/2021/01/SIPA_200_minijet_sn7-21.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/SIPA_200_minijet_sn7-21.jpg 500w, https://minijets.org/wp-content/uploads/2021/01/SIPA_200_minijet_sn7-21-300x191.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/SIPA_200_minijet_sn7-21-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/sipa-200-minijet/">Sipa S.200 Minijet</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Histoire du Sipa S.200 Minijet Dans les années 1950, la société française SIPA a développé le Sipa S.200 Minijet en collaboration avec Yves Gardan. Ce dernier avait entamé le projet GY-40 après avoir établi des contacts avec Turboméca. Le Minijet, un biplace d&#8217;entraînement mono-réacteur, se distingue par sa configuration bipoutre et sa taille réduite. Le [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/somers-kendall-sk-1/"><img loading="lazy" decoding="async" width="500" height="333" src="https://minijets.org/wp-content/uploads/2020/12/sk1-01.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2020/12/sk1-01.jpg 500w, https://minijets.org/wp-content/uploads/2020/12/sk1-01-300x200.jpg 300w, https://minijets.org/wp-content/uploads/2020/12/sk1-01-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/somers-kendall-sk-1/">Somers-Kendall SK-1</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Le Somers-Kendall SK-1 est un avion britannique, crée pour la course. Bien que pouvant être comparé au Fouga Midjet (avion en bois et turboréacteur Turbomeca Palas ), le Somers-kendall SK-1 s&#8217;en différencie par une conception plus avant-gardiste (4 ans plus tard il est vrai) et surtout biplace. L&#8217;histoire du Somers-Kendal SK-1, financé par Nat Somers et conçu par Hugh Kendall commence [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/varijet/"><img loading="lazy" decoding="async" width="500" height="333" src="https://minijets.org/wp-content/uploads/2022/02/Varijet_VH_DED_05.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2022/02/Varijet_VH_DED_05.jpg 500w, https://minijets.org/wp-content/uploads/2022/02/Varijet_VH_DED_05-300x200.jpg 300w, https://minijets.org/wp-content/uploads/2022/02/Varijet_VH_DED_05-18x12.jpg 18w" sizes="auto, (max-width: 500px) 100vw, 500px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/varijet/">VariJet</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Varieze equiped with a Turbomeca Palas Geoffrey&#8217;s Varijet project was to re-engine his&nbsp;Varieze&nbsp;with a&nbsp;Turbomeca Palas.&nbsp; Geoffrey Danes joined the SAAA (Sport Aircraft Association of Australia) in 1976 and built a Varieze (#2 in the air in Australia in Sept, 1979) His second project was a one of a kind composite aerobatic aircraft : the&nbsp;Maverick&nbsp;which was [&hellip;]</p>
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<h2 class="wp-block-heading">Autres Applications</h2>


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            <a href="https://minijets.org/en/150-300/turbomeca-palas/autres-utilisations/c-46palas/"><img loading="lazy" decoding="async" width="831" height="309" src="https://minijets.org/wp-content/uploads/2021/01/C46_Palas_03.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="Curtiss C-46 Commando Palas" srcset="https://minijets.org/wp-content/uploads/2021/01/C46_Palas_03.jpg 831w, https://minijets.org/wp-content/uploads/2021/01/C46_Palas_03-300x112.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/C46_Palas_03-768x286.jpg 768w, https://minijets.org/wp-content/uploads/2021/01/C46_Palas_03-18x7.jpg 18w" sizes="auto, (max-width: 831px) 100vw, 831px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/autres-utilisations/c-46palas/">Curtiss C-46 Commando</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Curtiss Turbomeca Palas turbojet assist engine is shown mounted on the wing of a Lloyd Aero Colombiano Curtiss C-46 Commando. This was the first time an installation of this type has been made for passenger service by a U.S. modification base. L.B. Smith Aicraft Corp., Miami. did the job. The turbojet flush intake nacelle was [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/autres-utilisations/douglas-dc-3/"><img loading="lazy" decoding="async" width="1302" height="523" src="https://minijets.org/wp-content/uploads/2021/01/DC3_Palas_01.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="DC3 - Palas" srcset="https://minijets.org/wp-content/uploads/2021/01/DC3_Palas_01.jpg 1302w, https://minijets.org/wp-content/uploads/2021/01/DC3_Palas_01-300x121.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/DC3_Palas_01-1024x411.jpg 1024w, https://minijets.org/wp-content/uploads/2021/01/DC3_Palas_01-768x308.jpg 768w, https://minijets.org/wp-content/uploads/2021/01/DC3_Palas_01-18x7.jpg 18w" sizes="auto, (max-width: 1302px) 100vw, 1302px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/autres-utilisations/douglas-dc-3/">Douglas DC3 Palas</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Le Douglas DC3 Palas était un projet de 1952, qui associait à un Douglas DC à un groupe d&#8217;appoint Palas de la SNCASO Douglas Douglas DC3 Palas avec son groupe d&#8217;appoint En&nbsp;1952,&nbsp;&nbsp;La SNCASO (Société Nationale de Constructions Aéronautiques du Sud-Ouest diffusait les résultats mesurés, en essais officiels et&nbsp;en exploitation, de son groupe d&#8217;appoint utilisant un [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/autres-utilisations/hydroglisseur-couzinet/"><img loading="lazy" decoding="async" width="300" height="200" src="https://minijets.org/wp-content/uploads/2021/01/Hydro_couzinet_mini.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Hydro_couzinet_mini.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Hydro_couzinet_mini-18x12.jpg 18w" sizes="auto, (max-width: 300px) 100vw, 300px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/autres-utilisations/hydroglisseur-couzinet/">Hydroglisseur Couzinet Palas</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Couzinet Ce n&#8217;est certes pas un avion, mais l&#8217;une des réalisations d&#8217;un grand ingénieur aéronautique français : René Couzinet. Il est propulsé par un turboréacteur Turbomeca Palas. On le voit ici navigant sur la Seine, aux environs de l&#8217;Ile de la Jatte, où était situé l&#8217;Usine et bureaux d&#8217;étude Couzinet.</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/autres-utilisations/sncaso-so30-bretagne/"><img loading="lazy" decoding="async" width="567" height="379" src="https://minijets.org/wp-content/uploads/2021/01/SO-30_bretagne_03.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="SO-30 P1 Bretagne Palas" srcset="https://minijets.org/wp-content/uploads/2021/01/SO-30_bretagne_03.jpg 567w, https://minijets.org/wp-content/uploads/2021/01/SO-30_bretagne_03-300x201.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/SO-30_bretagne_03-18x12.jpg 18w" sizes="auto, (max-width: 567px) 100vw, 567px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/autres-utilisations/sncaso-so30-bretagne/">SO-30 P1 Bretagne Palas</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>SNCASO L&#8217;histoire du SO-30 P1 Bretagne Palas commence dès&nbsp;mai 1941 lorsqu&#8217;une équipe de la SNCASO de Cannes commença, sous la direction de l&#8217;ingénieur Parot,&nbsp;l&#8217;étude d&#8217;un bimoteur de transport qu&#8217;on appelait alors le&nbsp;SO.30 Bellatrix. Le projet avança&nbsp;lentement et fut repris une fois la France libérée et la paix rétablie.&nbsp; Deux prototypes SO.30 N et SO.30 R [&hellip;]</p>
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<h2 class="wp-block-heading">Projets</h2>


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            <a href="https://minijets.org/en/150-300/turbomeca-palas/projets/airone-palas/"><img loading="lazy" decoding="async" width="800" height="573" src="https://minijets.org/wp-content/uploads/2022/09/Airone_palas_mini-1.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2022/09/Airone_palas_mini-1.jpg 800w, https://minijets.org/wp-content/uploads/2022/09/Airone_palas_mini-1-300x215.jpg 300w, https://minijets.org/wp-content/uploads/2022/09/Airone_palas_mini-1-768x550.jpg 768w, https://minijets.org/wp-content/uploads/2022/09/Airone_palas_mini-1-18x12.jpg 18w" sizes="auto, (max-width: 800px) 100vw, 800px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/projets/airone-palas/">Airone Jet</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Pasotti Spa Because of the Airone&#8217;s robustness, Stelio Frati has already drawn up the final plans for a version, called the Airone Jet, powered by two Turbomeca Palas. The only structural modification would&nbsp;be the use of a slightly thicker plywood skin on the wing which&nbsp;would bring the maximum permissible diving speed up to 340 m.p.h.&nbsp;Mr. [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/projets/dewoitine/"><img loading="lazy" decoding="async" width="412" height="201" src="https://minijets.org/wp-content/uploads/2020/12/Dewoitine_projet_Palas.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2020/12/Dewoitine_projet_Palas.jpg 412w, https://minijets.org/wp-content/uploads/2020/12/Dewoitine_projet_Palas-300x146.jpg 300w, https://minijets.org/wp-content/uploads/2020/12/Dewoitine_projet_Palas-18x9.jpg 18w" sizes="auto, (max-width: 412px) 100vw, 412px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/projets/dewoitine/">Dewoitine Avion Palas</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Iberavia En&nbsp;1954, Emile Dewoitine&nbsp;s&#8217;est intéressé, à&nbsp;la formule de l&#8217;école de début à réaction, en concevant un biplace propulsé par un réacteur de faible puissance. Il nous est parvenu sous le nom de Dewoitine Avion Palas. A l&#8217;image de ce qui a été fait par Yves Gardan avec le SIPA 200 Minijet et Stelio Frati avec [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/projets/fauvel-av-42/"><img loading="lazy" decoding="async" width="400" height="262" src="https://minijets.org/wp-content/uploads/2021/01/mini_AV42.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/mini_AV42.jpg 400w, https://minijets.org/wp-content/uploads/2021/01/mini_AV42-300x197.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/mini_AV42-18x12.jpg 18w" sizes="auto, (max-width: 400px) 100vw, 400px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/projets/fauvel-av-42/">Fauvel AV-42</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>En novembre 1952, Charles Fauvel dessina un avion à réaction de tourisme, propulsé par 3 turboréacteur Palas, le Fauvel AV-42. Cet appareil était conçu pour transporter 5 passagers à 500 km/h, sur une distance de 1000 à 3000 km. Trois réacteurs Turbomeca Palas alimentés par deux entrées d&#8217;air latérales et une ventrale devaient équiper l&#8217;AV-42, [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/projets/fouga-cm-72/"><img loading="lazy" decoding="async" width="400" height="267" src="https://minijets.org/wp-content/uploads/2021/01/Mini_fouga_CM72_02.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Mini_fouga_CM72_02.jpg 400w, https://minijets.org/wp-content/uploads/2021/01/Mini_fouga_CM72_02-300x200.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Mini_fouga_CM72_02-18x12.jpg 18w" sizes="auto, (max-width: 400px) 100vw, 400px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/projets/fouga-cm-72/">Fouga CM-72</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Fort de son expérience dans le domaine des planeurs propulsés par un réacteur, le bureau d&#8217;étude Fouga avait prévu de se lancer dans la construction du biplace Fouga CM-72 équipé d&#8217;un réacteur Turbomeca Palas. Le CM72, reprend la cellule et les ailes d&#8217;un CM-71. le turboréacteur est installé en pod, sur le dos du fuselage en [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/projets/fouga-cm-82-lutin/"><img loading="lazy" decoding="async" width="800" height="553" src="https://minijets.org/wp-content/uploads/2021/01/Fouga_cm82_lutin-01.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/Fouga_cm82_lutin-01.jpg 800w, https://minijets.org/wp-content/uploads/2021/01/Fouga_cm82_lutin-01-300x207.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/Fouga_cm82_lutin-01-768x531.jpg 768w, https://minijets.org/wp-content/uploads/2021/01/Fouga_cm82_lutin-01-18x12.jpg 18w" sizes="auto, (max-width: 800px) 100vw, 800px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/projets/fouga-cm-82-lutin/">Fouga CM-82 Lutin</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Etablissements FOUGA, Aire-sur-Adour les Projets Fouga CM-82 et CM-821 Lutin Le Fouga CM-82 Lutin a été présenté pour la première fois en juin 1951 au XIXème Salon de l&#8217;aéronautique&nbsp;qui se tenait pour la dernière année au grand Palais de Paris En&nbsp;1951, parallèlement à la conception du CM-170,&nbsp; le bureau d&#8217;études des Ets&nbsp;Fouga travail sur un [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/projets/kbl-12/"><img loading="lazy" decoding="async" width="492" height="294" src="https://minijets.org/wp-content/uploads/2021/01/KBL-12_01.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/KBL-12_01.jpg 492w, https://minijets.org/wp-content/uploads/2021/01/KBL-12_01-300x179.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/KBL-12_01-18x12.jpg 18w" sizes="auto, (max-width: 492px) 100vw, 492px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/projets/kbl-12/">KBL-12</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Konstrukcijski Biro Leov Le KBL-12 est un projet d&#8217;avion d&#8217;entrainement à réaction, étudié dans les années 50 par le KBL de Ljubljana dans l&#8217;ancienne Yougoslavie (actuelle Slovénie). Il a été conçu avec l&#8217;aide des jeunes ingénieurs de l&#8217;école Supérieur Technique de Ljubljana. On leur doit aussi les avions suivants : le LK-1, quadriplace de tourisme [&hellip;]</p>
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            <a href="https://minijets.org/en/150-300/turbomeca-palas/projets/payen-pa-149/"><img loading="lazy" decoding="async" width="285" height="142" src="https://minijets.org/wp-content/uploads/2021/01/pa149-01.jpg" class="attachment-post-thumbnail size-post-thumbnail wp-post-image" alt="" srcset="https://minijets.org/wp-content/uploads/2021/01/pa149-01.jpg 285w, https://minijets.org/wp-content/uploads/2021/01/pa149-01-18x9.jpg 18w" sizes="auto, (max-width: 285px) 100vw, 285px" /></a>
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            <h3 class="wp-block-getwid-custom-post-type__post-title"><a href="https://minijets.org/en/150-300/turbomeca-palas/projets/payen-pa-149/">Payen PA-149</a></h3>        </div>
        <div class="wp-block-getwid-custom-post-type__post-excerpt"><p>Le&nbsp;PAYEN Pa-149, étudié par Roland Payen, devait-être un biplace en tandem, biréacteurs, de sport. Il reprenait les dimensions du Pa-49 en les augmentant d&#8217;un facteur de 1:19, ce qui permettait en entre autre l&#8217;accueil du deuxième pilote. Ce dernier étant assis au centre de gravité de l&#8217;avion, aucune modification (triming) n&#8217;était nécessaire entre la configuration [&hellip;]</p>
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<h2 class="wp-block-heading">Sources and Notes</h2>



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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="400" height="438" src="http://minijets.org/wp-content/uploads/2021/01/Joseph_turbomeca.jpg" alt="Joseph Szydlowski" class="wp-image-2869" srcset="https://minijets.org/wp-content/uploads/2021/01/Joseph_turbomeca.jpg 400w, https://minijets.org/wp-content/uploads/2021/01/Joseph_turbomeca-274x300.jpg 274w, https://minijets.org/wp-content/uploads/2021/01/Joseph_turbomeca-11x12.jpg 11w" sizes="auto, (max-width: 400px) 100vw, 400px" /><figcaption class="wp-element-caption">Joseph Szydlowski</figcaption></figure>
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<h2 class="wp-block-heading">TURBOMECA</h2>



<p class="wp-block-paragraph">La société <strong>Turboméca </strong>a été crée en 1938 par MM. <strong>Szydlowski</strong> et <strong>Planiol </strong>afin d&#8217;assurer la conception et la réalisation de compresseurs et de turbines destinés à l&#8217;industrie aéronautique.<br><strong>Turboméca</strong> fait aujourd&#8217;hui partie du Groupe <strong>Safran</strong></p>



<p class="wp-block-paragraph">En 1947, sur commande du Ministère de l&#8217;Air, la société&nbsp;<strong>Turbomeca </strong>commence la réalisation d&#8217;une petite turbine à gaz destinée à l&#8217;entrainement d&#8217;un alternateur de bord. Cette turbine à gaz <strong>TT 782</strong> sera à l&#8217;origine du premier réacteur de la marque le TR 011, dont les premiers essai auront lieu en 1948, et la première application sous l&#8217;appellation&nbsp;Piméné&nbsp;se fera sur le planeur sylphe modifié le 14 juillet 1949.&nbsp;Le&nbsp;<strong>Palas</strong>, puis les&nbsp;Marbore&nbsp;I et II virent le jour en 1950. Dès cette date, et devant le succès de ses matériels, Turbomeca envisagea la conclusion d&#8217;accords de fabrication sous Licences qui concerneront, entre autres, les sociétés Blackburn au Royaume Unis et Continental Aviation &amp; Engineering Corporation aux Etats-Unis.</p>
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</div><p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/turbomeca-palas/">Turbomeca Palas</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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		<title>AMT Lynx</title>
		<link>https://minijets.org/en/150-300/amt-lynx/</link>
		
		<dc:creator><![CDATA[Philippe Bezard]]></dc:creator>
		<pubdate>Tue, 26 Jan 2021 17:02:35 +0000</pubdate>
				<category><![CDATA[Jet Engine 150-300]]></category>
		<guid ispermalink="false">http://tst.minijets.org/?page_id=2886</guid>

					<description><![CDATA[<p>The AMT&#160;Lynx&#160;is a direct &#8220;spin-off&#8221; of the successful Nike engine manufactured by AMT Netherlands.&#160;The engine is constructed around a single, fully in house CNC machined, radial compressor wheel and an axial flow turbine stage. The Lynx engine owns most of its excellent performance and power/weight ratio because of its revolutionary design diffuser stage similar to [&#8230;]</p>
<p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/amt-lynx/">AMT Lynx</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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										<content:encoded><![CDATA[<p class="wp-block-paragraph">The AMT&nbsp;Lynx&nbsp;is a direct &#8220;spin-off&#8221; of the successful Nike engine manufactured by <a href="https://amtjets.com/" data-type="URL" data-id="https://amtjets.com/" target="_blank" rel="noopener">AMT Netherlands</a>.&nbsp;The engine is constructed around a single, fully in house CNC machined, radial compressor wheel and an axial flow turbine stage. The Lynx engine owns most of its excellent performance and power/weight ratio because of its revolutionary design diffuser stage similar to the Nike engine.</p>



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<figure class="wp-block-image size-large"><img loading="lazy" decoding="async" width="700" height="525" src="http://minijets.org/wp-content/uploads/2021/01/AMT_lynx_01.jpg" alt="" class="wp-image-2583" srcset="https://minijets.org/wp-content/uploads/2021/01/AMT_lynx_01.jpg 700w, https://minijets.org/wp-content/uploads/2021/01/AMT_lynx_01-300x225.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/AMT_lynx_01-16x12.jpg 16w" sizes="auto, (max-width: 700px) 100vw, 700px" /><figcaption class="wp-element-caption">AMT Lynx. Source : text and picture are from AMT Netherlands</figcaption></figure>
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<h3 class="wp-block-heading">Starting system.</h3>



<p class="wp-block-paragraph">The Lynx engine is manufactured with an dual internal igniter system which allows a relaiable fully automatic start.</p>



<p class="wp-block-paragraph">Starting method : Direct kerosene starting gasturbine.</p>



<h3 class="wp-block-heading">Features.</h3>



<p class="wp-block-paragraph">A other feature used within the Lynx engine are the 2 internal EGT sensors, these 2 induvidual monitored EGT sensors (both a real Tt5) have both a small diameter of 1.5 mm, because of this small diameter there is a fast EGT response time possible. The result of this fast EGT response time is a short start up time of less than 45 seconds.</p>
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<h2 class="wp-block-heading">Application</h2>



<p class="wp-block-paragraph">This engine will find its use in large UAV high speed target drone applications, experimental aircraft, universities, sound studies, full size gliders and many more applications.</p>


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            <a href="https://minijets.org/en/150-300/amt-lynx/voodoo/">
        <img loading="lazy" decoding="async" width="960" height="650" src="https://minijets.org/wp-content/uploads/2021/01/xproject_voodoo_01.jpg" class="attachment-full size-full wp-post-image" alt="Voodoo personal jet" srcset="https://minijets.org/wp-content/uploads/2021/01/xproject_voodoo_01.jpg 960w, https://minijets.org/wp-content/uploads/2021/01/xproject_voodoo_01-300x203.jpg 300w, https://minijets.org/wp-content/uploads/2021/01/xproject_voodoo_01-768x520.jpg 768w, https://minijets.org/wp-content/uploads/2021/01/xproject_voodoo_01-18x12.jpg 18w" sizes="auto, (max-width: 960px) 100vw, 960px" />            </a>
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<h3 class="wp-block-getwid-template-post-title minijets_custom_title"><a class="wp-block-getwid-template-post-title__link" href="https://minijets.org/en/150-300/amt-lynx/voodoo/">Voodoo personal jet</a></h3>


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<div class="wp-block-getwid-template-post-content is-excerpt" ><p>Revelation Aerospace Le Voodoo Personal Jet est un avion monoplace développé par Revelation Aerospace, également connue sous le nom de Revelaero, basée à Jasper, Georgia, aux États-Unis. Conçu par Jeff Kerlo, cet appareil visait à offrir une expérience de vol personnelle avec des performances notables. Caractéristiques principales : Design : Le Voodoo adopte une configuration&hellip;</p></div>



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    <a href="https://minijets.org/en/150-300/amt-lynx/voodoo/" class="wp-block-button__link has-background has-white-background-color has-text-color has-vivid-cyan-blue-color">
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                    </div><p>L’article <a rel="nofollow" href="https://minijets.org/en/150-300/amt-lynx/">AMT Lynx</a> est apparu en premier sur <a rel="nofollow" href="https://minijets.org/en">Minijets</a>.</p>
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