Fabrication and testing of a leading-edge-shaped heat pipe-Reference-Cited by-同舟云学术

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Fabrication and testing of a leading-edge-shaped heat pipe

Published:1999-08-22 Issue: Volume: Page:
ISSN:
Container-title:9th International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Glass David¹,Camarda Charles²,Merrigan Michael³,Sena J.³,Reid Robert³

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

2. NASA, Johnson Space Center, Houston, TX

3. Los Alamos National Lab., NM

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-4866

Reference20 articles.

1. Four Space Shuttle Wing Leading Edge Concepts

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1. Numerical Simulation of Heat Pipe Thermal Performance for Aerospace Cooling System Applications;Aerospace;2024-01-17

2. Experimental Study On Gravity-effect for Startup Performance of High-Temperature Sodium Heat Pipe;Microgravity Science and Technology;2023-06-17

3. Heats pipes for temperature homogenization: A literature review;Applied Thermal Engineering;2017-05

4. Re-entry Aerothermal Environment Simulation of the TPS of Hypersonic Flight Vehicles;Astrophysics and Space Science Proceedings;2017

5. Thermal–structural analysis of the platelet heat-pipe-cooled leading edge of hypersonic vehicle;Acta Astronautica;2016-10

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