Solar Thermal Upper Stage technology demonstrator program-Reference-Cited by-同舟云学术

Solar Thermal Upper Stage technology demonstrator program

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
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Author:

Cady E.¹,Olsen A.¹

Affiliation:

1. McDonnell Douglas Aerospace, Huntington Beach, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3011

Reference5 articles.

1. Lin,C.S., Van Dresar, N.T., Hasan, M.M. "A Pressure Control Analysis of Cryogenic Storage Systems,"AIAA Paper-91-2405,June 1991.

2. Burge, G.W. "System Effects on Propellant Storability and Vehicle Performance," McDonnell Douglas Report DAC-59314 (AFRPL-TR-66-258), October 1966.

3. DiStefano, E., Cady, E.G., Rangel, R.H."Fill of Screen Liquid Acquisition Devices in Low Gravity Using a Thermodynamic Vent System," McDonnell Douglas Report MDC91H1086,August 1991.

4. Lester, D., Warner, M. "Gossamer Baggie Torus," Final Report PL-TR-93-3040, Phillips Lab, EAFB,CA, February 1994. Acknowledgments The authors wish to thank theSolar Thermal Upper Stage Technology Demonstrator Consortiummembers; United Applied Technologies-Concentrator; Thiokol-Concentrator Supports; NASA MSFCAbsorber/Engine, LH2Feed System Testing; NASA LeRC-Flight Type LH2Tank, Component Testing; USAF-PL (Edwards)-Concentrator/Engine Testing; and the University of Alabama Huntsville-Uncertainty Analysis.

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1. Solar thermal upper stage cryogen system engineering checkout test;35th Joint Propulsion Conference and Exhibit;1999-06-20

2. Solar thermal thruster made of single crystal molybdenum;Acta Astronautica;1997-07

3. Performance of LH2 storage and supply systems for advanced upper stages;32nd Joint Propulsion Conference and Exhibit;1996-07-01