Selection of a surface tension propellant management system for the Viking 75 Orbiter-Reference-Cited by-同舟云学术

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Selection of a surface tension propellant management system for the Viking 75 Orbiter

Published:1972-08-16 Issue: Volume: Page:
ISSN:
Container-title:8th Joint Propulsion Specialist Conference
language:
Short-container-title:

Author:

DOWDY M.¹,DEBROCK S.²

Affiliation:

1. California Institute of Technology, Jet Propulsion Laboratory, Propulsion Div., Pasadena, Calif.

2. Lockheed Missiles and Space, Inc., Sunnyvale, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1972-1042

Reference5 articles.

1. Igasventing __ Reliability I Confidence inbubble

2. THERMAL BLANKlT ISO.W-DIAM PAYLOADENVELO Fig. 1. Viking 1975 spacecraft

3. Fig. 4, Canr1-21 proCilo of haffle driving capability

Cited by 2 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. Development and Qualification of the Propellant Management System for Viking 75 Orbiter;Journal of Spacecraft and Rockets;1977-03

2. Surface tension propellant control for Viking 75 Orbiter;12th Propulsion Conference;1976-07-26

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