In view of the destructive ignitions that occur in hypergolic test firings of attitude-control motors under simulated high-altitude conditions, the preignition behavior of MMH, UDMH, A-50, and N2H4 with N2O4 was examined at low pressures and temperatures in the laboratory. (Author)
Preignition Products from Storable Propellants at Simulated High-Altitude Conditions
1967
46 pages
Report
No indication
English
Rocket Propellants , Rocket Engines & Motors , Storable propellants , Hypergolic rocket propellants , Autoignition , Captive tests , Starting , Damage , Combustion chambers , Attitude control systems , Rocket motors , High altitude , Nitrogen oxides , Altitude chambers , Dimethyl hydrazine (1-1) , Methyl hydrazines , Hydrazine , Infrared spectroscopy , Mass spectroscopy , Differential thermal analysis
Preignition characteristics of several fuels under simulated engine conditions
Engineering Index Backfile | 1941
|Earth-storable propellants for spacecraft.
NTRS | 1965
|