Shock interference peak heating measurements using phase change coatings-Reference-Cited by-同舟云学术

Shock interference peak heating measurements using phase change coatings

Published:1976-01 Issue:1 Volume:13 Page:61-63
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Keyes J. Wayne¹

Affiliation:

1. NASA Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.27884

Reference9 articles.

1. Optimum Launch Trajectories for the ATS-E Mission

2. Rocket trajectory optimization by a second- order numerical technique.

3. 3Rosenbaum, R. "A Combination of Numerical-Analytical Approach to Ascent Trajectory Optimization," AAS Science and Technology Series, Vol.11, American Astronautical Society, Washington, D.C., 1967, pp.243-262.

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