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In-Space Propulsion Assessment Processes and Criteria for Affordable SystemsIn a world of high launch costs to Low Earth Orbit (LEO), and of costs nearly twice as high to Geosynchronous Earth Orbit (GEO), it is clear that processes and criteria are required which will surface the path to greater affordability. Further, with propulsion systems making up a major part of the systems placed into multiple orbits, or beyond, it is clear that addressing propulsion systems for in-space propulsion (ISP) is a key part to breaking the barriers to affordable systems. While multitudes of Earth to Orbit transportation system efforts focus on reduced costs, the often neglected costs and related interactions of the in-space system equally require improvements that will enable broad end-to end customer affordability.
Document ID
20170011136
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Zapata, Edgar
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Rhodes, Russel
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
November 16, 2017
Publication Date
June 20, 1999
Subject Category
Spacecraft Design, Testing And Performance
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 99-2611
KSC-E-DAA-TN48227
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: Los Angeles, CA
Country: United States
Start Date: June 20, 1999
End Date: June 24, 1999
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
space propulsio
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