Aerothermal–Structural Analysis of a Rocket-Launched Mach 8 Scramjet Experiment: Descent-Reference-Cited by-同舟云学术

Aerothermal–Structural Analysis of a Rocket-Launched Mach 8 Scramjet Experiment: Descent

Published:2018-03 Issue:2 Volume:55 Page:501-517
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Capra Bianca R.¹,Brown L. M.²,Boyce R. R.²

Affiliation:

1. Queensland University of Technology, Brisbane, Queensland 4001, Australia

2. University of New South Wales Canberra, ACT, Canberra 2600, Australia

Funder

Australian Space Research Program

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33964

Reference21 articles.

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5. DottsR. L.CurryD. M.TillianD. J. “Orbiter Thermal Protection System,” Space Shuttle Technical Conference, NASA CP 2342, Part 2, 1985, pp. 1062–1081.

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