The Phenomena of Combustion Instability in Bipropellant Rocket Engines Using NTO/Hydrazine-sorts
55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law ; 2004 ; Vancouver , British Columbia , Canada
2004-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Bipropellant rocket engines for Shuttle payloads
AIAA | 1979
|Injector for bipropellant rocket engines Patent
NTRS | 1964
|