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The Status of Spacecraft Bus and Platform Technology Development under the NASA In-Space Propulsion Technology ProgramNASA's In-Space Propulsion Technology (ISPT) program has been developing technologies for lowering the cost of planetary science missions. The technology areas include electric propulsion technologies, spacecraft bus technologies, entry vehicle technologies, and design tools for systems analysis and mission trajectories. The electric propulsion technologies include critical components of both gridded and non-gridded ion propulsion systems. The spacecraft bus technologies under development include an ultra-lightweight tank (ULTT) and advanced xenon feed system (AXFS). The entry vehicle technologies include the development of a multi-mission entry vehicle, mission design tools and aerocapture. The design tools under development include system analysis tools and mission trajectory design tools.
Document ID
20140000475
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Anderson, David
(NASA Glenn Research Center Cleveland, OH, United States)
Pencil, Eric J.
(NASA Glenn Research Center Cleveland, OH, United States)
Glaab, Louis
(NASA Langley Research Center Hampton, VA, United States)
Falck, Robert D.
(NASA Glenn Research Center Cleveland, OH, United States)
Dankanich, John
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
January 29, 2014
Publication Date
June 17, 2013
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN9787
Report Number: GRC-E-DAA-TN9787
Meeting Information
Meeting: International Planetary Probe Workshop
Location: San Jose, CA
Country: United States
Start Date: June 17, 2013
End Date: June 21, 2013
Sponsors: San Jose State Univ.
Funding Number(s)
WBS: WBS 346620.01.13.01.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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