The paper proposes a modular approach to rocket propulsion which offers a versatile method for realizing the goals of low cost, safety, reliability, and ease of operation. It is shown that, using practical modules made up of only 4-6 individual elements, it is possible to achieve thrust levels of 2-3 mln lbf and more, using turbomachinery, thrust chambers, lines, and valves about the size of SSME hardware. The approach is illustrated by a LOX/LH2 configuration.
Integrated modular propulsion for launch vehicles
AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit ; 1993 ; Monterey, CA, United States
1993-06-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Integrated modular propulsion for launch vehicles
AIAA | 1993
|Propulsion technology for modular expendable launch vehicles
Tema Archiv | 1987
|Propulsion for Future Launch Vehicles
British Library Conference Proceedings | 1993
|Propulsion for future launch vehicles
AIAA | 1993
|