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The Status of Spacecraft Bus and Platform Technology Development Under the NASA ISPT ProgramThe In-Space Propulsion Technology (ISPT) program is developing spacecraft bus and platform technologies that will enable or enhance NASA robotic science missions. The ISPT program is currently developing technology in three areas that include Propulsion System Technologies, Entry Vehicle Technologies, and Systems Mission Analysis. ISPTs propulsion technologies include: 1) NASAs Evolutionary Xenon Thruster (NEXT) ion propulsion system, a 0.6-7 kW throttle-able gridded ion system; 2) a Hall-effect electric propulsion (HEP) system for sample return and low cost missions; 3) the Advanced Xenon Flow Control System (AXFS); ultra-lightweight propellant tank technologies (ULTT); and propulsion technologies for a Mars Ascent Vehicle (MAV). The AXFS and ULTT are two component technologies being developed with nearer-term flight infusion in mind, whereas NEXT and the HEP are being developed as EP systems. ISPTs entry vehicle technologies are: 1) Aerocapture technology development with investments in a family of thermal protection system (TPS) materials and structures; guidance, navigation, and control (GNC) models of blunt-body rigid aeroshells; and aerothermal effect models; and 2) Multi-mission technologies for Earth Entry Vehicles (MMEEV) for sample return missions. The Systems Mission Analysis area is focused on developing tools and assessing the application of propulsion, entry vehicle, and spacecraft bus technologies to a wide variety of mission concepts. Several of the ISPT technologies are related to sample return missions and other spacecraft bus technology needs like: MAV propulsion, MMEEV, and electric propulsion. These technologies, as well as Aerocapture, are more vehicle and mission-focused, and present a different set of technology development challenges. These in-space propulsion technologies are applicable, and potentially enabling for future NASA Discovery, New Frontiers, Flagship and sample return missions currently under consideration. This paper provides a brief overview of the ISPT program, describing the development status and technology infusion readiness.
Document ID
20140012555
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Anderson, David
(NASA Glenn Research Center Cleveland, OH United States)
Munk, Michelle M.
(NASA Langley Research Center Hampton, VA United States)
Pencil, Eric
(NASA Glenn Research Center Cleveland, OH United States)
Dankanich, John
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Glaab, Louis
(NASA Langley Research Center Hampton, VA United States)
Peterson, Todd
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 24, 2014
Publication Date
March 1, 2014
Subject Category
Technology Utilization And Surface Transportation
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN12666
Report Number: GRC-E-DAA-TN12666
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 1, 2014
End Date: March 8, 2014
Sponsors: American Inst. of Aeronautics and Astronautics, Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: WBS 346620.01.13.01.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
electric propulsion
entry vehicles
systems analysis
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