Technical studies show major advantages in propulsion system flexibility, simplicity, reliability, and cost effectiveness attained through use of common propellants for all propulsion functions on cryogenic space vehicles; design considerations involved in development of auxiliary propulsion systems using cryogenic propellants and applicability of catalyst and spark igniter units to oxygen-hydrogen thrust chambers for pulse-mode operations are discussed. (31362)
Cryogenic auxiliary propulsion systems
ASME Aviation Space -- Progress Prospects
ASME -- Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Propulsion systems
1968
7 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Satellite auxiliary propulsion systems
NTRS | 1973
|NTRS | 1984
|AIAA | 1971
|NTIS | 2011
|NTRS | 1971
|