Small Launch Vehicle Concept Development for Affordable Multi-Stage Inline Configurations-Reference-Cited by-同舟云学术

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Small Launch Vehicle Concept Development for Affordable Multi-Stage Inline Configurations

Published:2013-09-10 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2013 Conference and Exposition
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Author:

Beers Benjamin R.¹,Waters Eric¹,Philips Alan¹,Threet Grady¹

Affiliation:

1. NASA Marshall Space Flight Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-5529

Reference6 articles.

1. 1"DeltaIVPayloadPlanner'sGuide,"Sept.2007,URL: www.ulalaunch.com/site/./guides/DeltaIVPayloadPlannersGuide2007.pdf

2. 4Hill,P.G.,andPeterson,C.R.,MechanicsandThermodynamicsofPropulsion,2nded.,Addison-Wesley,1992,pp.571.

3. 5Turner,R.E.,andHill,C.K."TerrestrialEnvironment(Climactic)CriteriaGuidelinesfor UseinAerospaceVehicle Development,"NASA TM-82473, 1982.

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. Application of Design of Experiments and Surrogate Modeling within the NASA Advanced Concepts Office, Earth-to-Orbit Design Process;AIAA SPACE 2016;2016-09-09

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