The test article, test approach, data analysis and results of a study undertaken to characterize performance of the augmentation section of the Rocket Research Company Augmented Catalytic Thruster as a gas resistojet using hydrogen, nitrogen and ammonia as propellants are described. This renewed interest in resistojets is a result of propulsion systems definition studies which indicate potential application to space station auxiliary propulsion.
Radiative resistojet performance characterization tests
1984-09-01
Report
No indication
English
Radiative Resistojet Performance Characterization Tests
NTIS | 1984
|Ten-millipound resistojet performance.
NTRS | 1968
|Ten-millipound resistojet performance.
AIAA | 1968
|Ten-millipound resistojet performance
AIAA | 1967
|