LOX/hydrocarbon rocket engine analytical design methodology development and validation. Volume 2: Appendices

This final report includes a discussion of the work accomplished during the period from Dec. 1988 through Nov. 1991. The objective of the program was to assemble existing performance and combustion stability models into a usable design methodology capable of designing and analyzing high-performance...

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Bibliographische Detailangaben

Hauptverfasser:	Niiya, Karen E., Walker, Richard E., Pieper, Jerry L., Nguyen, Thong V.
Format:	Report
Sprache:	eng
Schlagworte:	Spacecraft Propulsion And Power
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