Reduction of Aerodynamic Interference for Separation of Two-Stage Reuseable Launch Vehicles
Author:
Affiliation:
1. Kyushu University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1101
Reference3 articles.
1. Wayne J. Bordelon, Jr., Alonzo L. Frost, Darren K. Reed, "STAGE SEPARATION WIND TUNNEL TESTS OF A GENERIC TWO-STAGE-TO-ORBIT LAUNCH VEHICLE", AIAA Paper 2003-4227.
2. Kelly J. Murphy, William I. Scallion, "Experimental Stage Separation Tool Development in NASA Langley's Aerothermodynamics Laboratory", AIAA Paper 2005-6127.
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