Magnetohydrodynamic energy bypass applications for single stage-to-orbit vehicles

33rd Plasmadynamics and Lasers Conference

Volumn , Issue , 2002, Pages

  Lee, Ying Ming ^a   Czysz, Paul A ^b   Petley, Dennis ^c   Hunt, James L ^c  

^a MSE Technology Applications Incorporated   (United States)

^b HyperTech Concepts   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

MAGNETOHYDRODYNAMICS; NASA; RESEARCH;

AMES RESEARCH CENTERS; HYPERSONIC FLIGHT VEHICLES; NASA LANGLEY RESEARCH CENTER; OPERATIONAL CONCEPTS; POLITICAL STRUCTURE; SMALL BUSINESS INNOVATIVE RESEARCHES; TECHNOLOGY APPLICATION; TOTAL SYSTEM PERFORMANCE;

HYPERSONIC VEHICLES;

EID: 84896057578     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. C. Park, U. Mehta, and D. Bogdanoff, Theoretical Performance of a MHD-Bypass Scramjet with Nonequilibrium Ionization, NASA TM-2001- 210918, NASA Ames Research Center, Moffett Field, California, June 2001.
2. Y. Lee, P. A. Czysz, and D. Petley, Magnetohydrodymnamic Energy Bypass Applications for Single Stage-to-Orbit Vehicles, AIAA Paper #2001-1901, presented at the AIAA/NAL-NASDA-ISAS 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, April 2001.
3. C.H. Builder, On the Thermodynamic Spectrum of Airbreathing Propulsion, AIAA Paper #64-243, 1st AIAA Annual Meeting, Washington, D.C., July 1964.
4. C. Bruno and P.A. Czysz, Fuel Reforming for Future RBCC Vehicles, Presented at the XIV ISABE Symposium, Florence, Italy, Sept. 1999.