Design and Flight Testing of a Reciprocating Pump Fed Rocket-Reference-Cited by-同舟云学术

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Design and Flight Testing of a Reciprocating Pump Fed Rocket

Published:1994-06-27 Issue: Volume: Page:
ISSN:
Container-title:30th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

WHITEHEAD JOHN¹,PITTENGER LEE¹,COLELLA NICHOLAS¹

Affiliation:

1. LAWRENCE LIVERMORE NATIONAL LABORATORY, LIVERMORE, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3031

Reference8 articles.

1. Whitehead, J.C., EreePiston PumpsforMiniatureRocket &Q&iQLAIAA 91-1837,1991. A h UCRL-JC-107465. 4. Maybee,J.C.,G,T.Brewster,D.G.Swink.TestResultsaf a Pumd MonomopellantProDulsionSystem,Praceedingsof the 1992 Joint Army Navy NASA Air Force (JANNAF) PropulsionMeeting (CPIA Publication 580),VolumeI, p. 65, 1992.

2. e ve * V ' e Proceedings of the 1992 JANNAF

3. Whitehead,J.C. t wth hmus,AIAA 9 3 - 2 l w - J C - 1 1-

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1. Technology and Hardware;History of Liquid Propellant Rocket Engines;2006-01

2. Reciprocating Pump Systems for Space Propulsion;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26

3. Launch Vehicle and Spacecraft System Design Using the Pistonless Pump;Space 2004 Conference and Exhibit;2004-06-19

4. High-Pressure-Pumped Hydrazine for Mars Sample Return;Journal of Spacecraft and Rockets;2000-07

5. Mars ascent propulsion options for small sample return vehicles;33rd Joint Propulsion Conference and Exhibit;1997-07-06

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