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
55 pages
Report
Keine Angabe
Englisch
Radiative resistojet performance characterization tests
NTRS | 1984
|Ten-millipound resistojet performance.
NTRS | 1968
|Ten-millipound resistojet performance.
AIAA | 1968
|Ten-millipound resistojet performance
AIAA | 1967
|