Hypersonic MHD propulsion system integration for a manned laser-boosted transatmospheric aerospacecraft

Author:

Myrabo L,Head D,Rajzer Y,Surzhikov S,Rosa R

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. Propulsion System Using a Cavity Reactor and Magnetohydrodynamic Generator

2. Rosa, R.J. "The Application of Magnetohydrodynamic Generators in Nuclear Rocket Propulsion", AERL Research Report 111, AFBSD-TR-61-58,ContractNo. AFW(647)-278, Avco-EverettResearchLaboratory,Everett, MA, Aug. 1961.

3. Magnetohydrodynamic Generators and Nuclear Propulsion

4. Analysis and design of an ultrahigh temperature hydrogen-fueled MHD generator

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1. MHD hypersonic flow control for aerospace applications;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14

2. Experimental investigation of a 2-D MHD slipstream accelerator - Progress report;37th Joint Propulsion Conference and Exhibit;2001-07-08

3. Experimental investigation of an electric arc air-spike with and without blunt body in hypersonic flow;39th Aerospace Sciences Meeting and Exhibit;2001-01-08

4. Experimental investigation of a 2-D MHD slipstream accelerator and generator;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24

5. Experimental investigation of a 2-D MHD slipstream generator and accelerator with freestream Mach = 7.6 and T(0) = 4100 K;38th Aerospace Sciences Meeting and Exhibit;2000-01-10

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