Space Launch System Base Heating Test: Experimental Operations and Results-Reference-Cited by-同舟云学术

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Space Launch System Base Heating Test: Experimental Operations and Results

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Dufrene Aaron T.¹,Mehta Manish²,MacLean Matthew G.¹,Seaford Mark²,Holden Michael S.¹

Affiliation:

1. CUBRC

2. NASA Marshall Space Flight Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0546

Reference16 articles.

1. Space Launch System Base Heating Test: Environments and Base Flow Physics

2. Vidal, R. J. "Model Instrumentation Techniques for Heat Transfer and Force Measurements in a Hypersonic Shock Tunnel." Cornell Aeronautical Laboratory Report AD-917-A-1, 1956.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Base Thermal Environment on Multinozzle Rocket Configurations;Journal of Spacecraft and Rockets;2022-11

2. Seeding Method for Velocimetry and Visualization of Supersonic Retropropulsion Nozzle Plumes;AIAA SCITECH 2022 Forum;2022-01-03

3. Space Launch System Base Heating Test: Tunable Diode Laser Absorption Spectroscopy;54th AIAA Aerospace Sciences Meeting;2016-01-02

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