Il s’agit un projet de turboréacteur devant équiper un monoplace à réaction conçu par les professeurs et les étudiants du Cal-aero Technical Institute of California en 1949. Un premier prototype, équipé d’une large chambre à combustion verticale a été expérimenté. Par contre nous n’avons aucune information sur le modèle définitif.
Description
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IS system
USCS system
Manufacturer | Cal-Aero |
Country | United States of America |
Model | Cal-Aero jet engine |
Initial testing | 1949 |
Certification | .. |
End of production | . |
Nb build | |
Type | Turboréacteur à simple flux |
Constitution
Combustion chamber |
HPC | nb of HP compressor stages | 1C |
HPT | nb of HP turbine stages | 1 |
Dimensions
Diameter | mm |
Length | mm |
Weight
Dry | kg |
Complete | kg |
Performances
Maximum RPM | t/mn | |
Continuous maximum RPM | t/mn | |
Idle speed | t/mn | |
Maximum thrust | 109,0 kgp | |
Continuous maximum thrust | kgp | |
Idle thrust | kgp | |
EGT max. | °C | |
Pressure ratio | ||
Total flow rate |
Consumption
Maximum specific consumption | kg/kgp-h |
Cruise specific consumption | kg/kgp-h |
Manufacturer | Cal-Aero |
Country | United States of America |
Model | Cal-Aero jet engine |
Initial testing | 1949 |
Certification | .. |
End of production | . |
Nb build | |
Type | Turboréacteur à simple flux |
Constitution
Combustion chamber |
HPC | nb of HP compressor stages | 1C |
HPT | nb of HP turbine stages | 1 |
Dimensions
Diameter | |
Length |
Weight
Dry | |
Complete |
Performances
Maximum RPM | ||
Continuous maximum RPM | ||
Idle speed | ||
Maximum thrust | 240.30 lbs | |
Continuous maximum thrust | ||
Idle thrust | ||
EGT max. | ||
Pressure ratio | ||
Total flow rate |
Consumption
Maximum specific consumption | |
Cruise specific consumption |