The design and evolution of the Beta two-stage-to-orbit horizontal takeoff and landing launch system
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
2. USAF, Wright Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-5080
Reference3 articles.
1. Figure 19. Year 2005 Launch Vehicle Architecture
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