Hyper-X Research Vehicle (HXRV) experimental aerodynamics test program overview

Author:

Holland Scott1,Woods William1,Engelund Walter1

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Investigation on Dynamic Derivative Test Technique in Hypersonic Wind Tunnel;Lecture Notes in Electrical Engineering;2019

2. Separation Analysis of Launch Vehicle Crew Escape Systems;22nd Applied Aerodynamics Conference and Exhibit;2004-06-20

3. Stage Separation Analysis of the X-43A Research Vehicle;22nd Applied Aerodynamics Conference and Exhibit;2004-06-20

4. Hyper-X program status;10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference;2001-04-24

5. Hyper-X program status;39th Aerospace Sciences Meeting and Exhibit;2001-01-08

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