Rocket engines with nitrogen tetroxide/hydrazine injectors destructive instability due to pressure disturbances, establishing origin, propagations velocity and pops extent by streak photography
Popping phenomena with N2O4/N2H4 injectors
FALL MEETING ON THE PERSPECTIVE OF SST AIRCRAFT NOISE PROBLEM ; 1970 ; PASADENA, CA
1970-10-01
Conference paper
No indication
English
Development and Demonstration of a N2O4/N2H4 Injector
NTIS | 1969
|NTRS | 1986
|Die Dampfdichte dissociierender N2O4-Dämpfe
TIBKAT | 1905
|