论文信息 - Integrating Aeroheating and TPS into Conceptual RLV Design - 字舞流文

Integrating Aeroheating and TPS into Conceptual RLV Design

9th International Space Planes and Hypersonic Systems and Technologies Conference Norfolk, VA, November 1-5, 1999.

John R. Olds | Karl K. Cowart

[1] John Rutherford,et al. American institute of aeronautics and astronautics graduate design competitions , 1996 .

[2] I. O. Macconochie,et al. Techniques for the determination of mass properties of earth-to-orbit transportation systems , 1978 .

[3] R. L. Dotts,et al. Comparison of Orbiter STS-2 Development Flight Instrumentation Data with Thermal Math Model Predictions , 1982 .

[4] D. R. Komar,et al. Stargazer: A TSTO Bantam-X Vehicle Concept Utilizing Rocket-Based Combined Cycle Propulsion , 1999 .

[5] J. E. Pond,et al. MINIVER upgrade for the AVID system. Volume 3: EXITS user's and input guide , 1983 .

[6] John R. Olds. Launch vehicle systems analysis , 1999 .