Review of NASA's Hypersonic Research Engine Project

Author:

ANDREWS EARL1,MACKLEY ERNEST2

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

2. Analytical Services and Materials, Inc., Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Cited by 7 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 low total temperature combustion characteristics of kerosene-fueled supersonic combustor;Chinese Journal of Aeronautics;2021-11

2. Design and cold flow test of a scramjet nozzle with nonuniform inflow;Acta Astronautica;2015-03

3. Hypersonic Inlet Flow Analysis at Mach 5, 6 and 7;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

4. Two Options for Flight Testing Rocket-Based Combined-Cycle Engines;Journal of Spacecraft and Rockets;1999-09

5. On the bridge from hypersonic aeropropulsion ground test data to flight performance;20th AIAA Advanced Measurement and Ground Testing Technology Conference;1998-06-15

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