Development of a Propellant Management Device (PMD) for Restartable Future Cryogenic Upper Stages-Reference-Cited by-同舟云学术

Development of a Propellant Management Device (PMD) for Restartable Future Cryogenic Upper Stages

Published:2006-07-09 Issue: Volume: Page:
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Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Behruzi Philipp,Michaelis Mark

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. 2Behruzi, K. P., and Netter, G. "Concept Analysis of PMD Designs for Future Upper Stages", 54th Int. Astronautical Congress, Bremen, Sept.Oct.2003

2. 4Netter,G.,andDreyer,M."FluidMechanicsApplicationfortheDesignandTestoftheNewGenerationofSurfaceTension Tank(OST-2), 1stEuropean Symposium"Fluidsin Space", p.179-193,Ajaccio,France, Nov. 1991

3. 8"Low Gravity Propellant Control using Capillary Devices in Large Scale Cryogenic Vehicles", Contract NAS 8-21465,Convair Divisionof General Dynamics, Aug. 1970

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