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Liquid and Solid Propulsion Systems Attributes - Unique, Common and ComplementaryIn this study, attributes are described for solid and liquid propulsion systems based on historical data. This study is not intended to compare liquid and solid propulsion system attributes, rather to present options for their use in various mission scenarios. US launch vehicle data from 1970 to 2008 was analyzed to assess solid and liquid propulsion development cost and schedule characteristics, performance features, and safety and mission success attributes. The study assessed historical trends for liquid and solid systems, and investigated implications of those trends. It was found that the two propulsion technologies have unique, common and complementary attributes that can be leveraged to meet mission requirements.
Document ID
20140010912
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Cannon, James L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lampton, Pat
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Williams, Thomas J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 22, 2014
Publication Date
May 19, 2014
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M14-3376
Report Number: M14-3376
Meeting Information
Meeting: JANNAF Propulsion Meeting
Location: Charleston, SC
Country: United States
Start Date: May 19, 2014
End Date: May 22, 2014
Sponsors: Department of the Air Force, NASA Headquarters, Department of the Navy, Department of the Army
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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