Venus Lander Electronics Payload Thermal Management Using a Multi-stage Refrigeration System-Reference-Cited by-同舟云学术

Venus Lander Electronics Payload Thermal Management Using a Multi-stage Refrigeration System

Published:2017-06-02 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Thermophysics Conference
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Author:

Anderson Kevin R.¹,McNamara Christopher¹,Gatti Ariel²

Affiliation:

1. California State Polytechnic University, Pomona

2. Ingenium Technical Services, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4344

Reference34 articles.

1. Progress in Astronautics and Aeronautics;Hennis L. A.,1978

2. Venus surface power and cooling systems

3. Pauken, M, Emis, N., van Luvender, M., Polk, J. and Del Castillo, L. "Thermal Control Technology Developments for a Venus Lander," Space, Propulsion & Energy Sciences Intl. Forum SPESIF-2010: 14th Conference on Thermophysics Applications in Microgravity, 7th Symposium on New Frontiers in Space Propulsion Sciences 2nd Symposium on Astrosociology, 1st Symposium on High Frequency Gravitational Waves. AIP Conference Proceedings, Vol. 1208, pp. 68-75, 2010.

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