Propulsion and aerodynamic analysis of the Beta II two-stage-to-orbit vehicle
Author:
Affiliation:
1. Sverdrup Technology, Inc., Brook Park; NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-4245
Reference19 articles.
1. Midea,A.C. "Mach 6.5Air Induction System Design for the Beta IITwo-Stage-To-OrbitBooster Vehicle",AIAA 91-3196,October 1991.
2. SnyderC.A.; MaldonadoJ.J. 'The Design and Performance Estimates for the Propulsion Module for the Booster of a TSTO Vehicle", AIAA 91-3136,September,1991.
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