Effect of lift-to-drag ratio in pilot rating of the HL-20 landing task
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. Lockheed Engineering & Sciences Company, Hampton, Virginia 2366
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25564
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2. A reusable space vehicle design study exploring sharp leading edges;35th AIAA Thermophysics Conference;2001-06-11
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4. Design strategies for a winged-body rocket SSTO;33rd Aerospace Sciences Meeting and Exhibit;1995-01-09
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