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Performance Modeling of Launch Vehicles Utilizing Vapor Pressure (Vapak) Based Propulsion Systems

机译：基于蒸气压（Vapak）的推进系统对运载火箭的性能建模

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来源
《Space 2006》|2006年|P.1-11|共11页
会议地点 San Jose CA(US)
作者
R. Ewig; B. McKinney; G. Hudson;
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作者单位

AirLaunch LLC, Kirkland, WA;

AirLaunch LLC, Kirkland, WA;

AirLaunch LLC, Kirkland, WA;

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会议组织
原文格式 PDF
正文语种
中图分类航空、航天技术的研究与探索;
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4. Performance Modeling of Launch Vehicles Utilizing Vapor Pressure (Vapak) Based Propulsion Systems [C] . Space . 2006

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Performance Modeling of Launch Vehicles Utilizing Vapor Pressure (Vapak) Based Propulsion Systems

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