NASA NTRS · 19840025391
Radiative resistojet performance characterization tests
Abstract
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.
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Miyake, C. I.. 1984-09-01. Radiative resistojet performance characterization tests. https://ntrs.nasa.gov/citations/19840025391
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