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REUSABLE PROPULSION ARCHITECTURE FOR SUSTAINABLE LOW-COST ACCESS TO SPACEThe primary obstacle to any space-based mission is, and has always been, the cost of access to space. Even with impressive efforts toward reusability, no system has come close to lowering the cost a significant amount. It is postulated here, that architectural innovation is necessary to make reusability feasible, not incremental subsystem changes. This paper shows two architectural approaches of reusability that merit further study investments. Both #inherently# have performance increases and cost advantages to make affordable access to space a near term reality. A rocket launched from a subsonic aircraft (specifically the Crossbow methodology) and a momentum exchange tether, reboosted by electrodynamics, offer possibilities of substantial reductions in the total transportation architecture mass - making access-to-space cost-effective. They also offer intangible benefits that reduce risk or offer large growth potential. The cost analysis indicates that approximately a 50% savings is obtained using today#s aerospace materials and practices.
Document ID
20060004772
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Bonometti, J. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Dankanich, J. W.
(Gray Research, Inc. Huntsville, AL, United States)
Frame, K. L.
(Gray Research, Inc. Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 2005 Joint Army Navy Nasa Air Force (JANNAF) Conference
Location: Monterey, CA
Country: United States
Start Date: December 5, 2005
End Date: December 8, 2005
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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