NASA's dual-fuel airbreathing hypersonic vehicle study

Author:

Hunt James1,Eiswirth Edward2

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

2. McDonnell Douglas Aerospace, Saint Louis, MO

Publisher

American Institute of Aeronautics and Astronautics

Reference1 articles.

Cited by 13 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. A Rapid Method of Integrated Aeropropulsive Analysis for the Conceptual Design of Airbreathing Hypersonic Aircraft;Aerospace;2024-01-18

2. Uncertainty Propagation in Integrated Airframe–Propulsion System Analysis for Hypersonic Vehicles;Journal of Propulsion and Power;2015-01

3. Flight-Test-Determined Aerodynamic Force and Moment Characteristics of the X-43A at Mach 7.0;14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference;2006-06-15

4. Overview With Results and Lessons Learned of the X-43A Mach 10 Flight;AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference;2005-05-16

5. A Chief Engineer's View of the NASA X-43A Scramjet Flight Test;AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference;2005-05-16

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