Transient analysis of pressurization and pneumatic subsystems of the X-34 main propulsion system-Reference-Cited by-同舟云学术

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Transient analysis of pressurization and pneumatic subsystems of the X-34 main propulsion system

Published:2000-07-24 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Hedayat A.¹,Knight K.¹,Champion, Jr. R.²

Affiliation:

1. Sverdrup Technology, Inc., Huntsville, AL

2. NASA, Marshall Space Flight Center, Huntsville, AL

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3720

Reference6 articles.

1. X-34 propulsion system design

2. Champion,R.H.,Jr., andDarrow,R.I, Jr.(1998), "X-34 Main Propulsion System Design and Operation,"AIAApaperNo.AIAA-98-4032.

3. Propellant management and conditioning within the X-34 Main Propulsion System

4. McDonald, J. P., Minor, R. B., Knight, K. C., Russell, F.I, Jr., andChampion,R.H.,Jr.(1998), "Propellant Feed Subsystem for the X-34Main Propulsion System," AIAA paper No. AIAA-98-3517.

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1. Simulink Model of the Ares I Upper Stage Main Propulsion System;AIAA Modeling and Simulation Technologies Conference and Exhibit;2008-06-15

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