A Methodology to Rapidly and Effectively Assess the Reliability of Conceptual Advanced Rocket Engines-Reference-Cited by-同舟云学术

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A Methodology to Rapidly and Effectively Assess the Reliability of Conceptual Advanced Rocket Engines

Published:2004-06-26 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Maggio Gaspare¹,Sen D¹,Hark F¹

Affiliation:

1. Science Applications International Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3515

Reference5 articles.

1. 1NASAQRAS2000SSMERiskEstimate,NASAHeadquarters,2000.

2. 2Biggs,R."SSMEReliabilityDetermination",Rocketdyne,31July2003.

3. 4Visser,BandMaggio,G."ADynamicProbabilisticRiskModelAppliedtotheSpaceShuttleMainEngine,"PSAM,1998.

4. 5Maggio, G., and Pelaccio, D., G. "Factors And Metrics In Establishing Reliability Goals For Next Generation Launch VehicleLiquidPropulsionSystems,"JPC,2000.

Cited by 1 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. Integrated Design Methodology for Highly Reliable Liquid Rocket Engine;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2006

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