An airbreathing launch vehicle design with turbine-based lowspeed propulsion and dual mode scramjet high-speed propulsion
Author:
Affiliation:
1. FDC/NYMA, Inc., Aerospace Sector, Hampton, VA
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-4948
Reference8 articles.
1. Hunt, J.L. "Airbreathing / Rocket Single-Stageto-Orbit Design Matrix0022, AIAA 95-6011, April 1995.
2. Adaptive Modeling Language, Version 3.1.2, TechnoSoft, Inc. Cincinnati, OH. Copyright 1999.
3. ,y~-MA, Copyright 1988-1998.
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