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NASA In-Space Propulsion Technologies and Their Infusion PotentialThe In-Space Propulsion Technology (ISPT) program has been developing in-space propulsion technologies that will enable or enhance NASA robotic science missions. The ISPT program is currently developing technology in four areas that include Propulsion System Technologies (Electric and Chemical), Entry Vehicle Technologies (Aerocapture and Earth entry vehicles), Spacecraft Bus and Sample Return Propulsion Technologies (components and ascent vehicles), and Systems/Mission Analysis. Three technologies are ready for flight infusion: 1) the high-temperature Advanced Material Bipropellant Rocket (AMBR) engine providing higher performance; 2) NASA s Evolutionary Xenon Thruster (NEXT) ion propulsion system, a 0.6-7 kW throttle-able gridded ion system; and 3) Aerocapture technology development with investments in a family of thermal protection system (TPS) materials and structures; guidance, navigation, and control (GN&C) models of blunt-body rigid aeroshells; and aerothermal effect models. Two component technologies that will be ready for flight infusion in the near future will be Advanced Xenon Flow Control System, and ultra-lightweight propellant tank technologies. Future focuses for ISPT are sample return missions and other spacecraft bus technologies like: 1) Mars Ascent Vehicles (MAV); 2) multi-mission technologies for Earth Entry Vehicles (MMEEV) for sample return missions; and 3) electric propulsion for sample return and low cost missions. These technologies are more vehicle-focused, and present a different set of technology infusion challenges. While the Systems/Mission Analysis area is focused on developing tools and assessing the application of propulsion technologies to a wide variety of mission concepts. These in-space propulsion technologies are applicable, and potentially enabling for future NASA Discovery, New Frontiers, and sample return missions currently under consideration, as well as having broad applicability to potential Flagship missions. This paper provides a brief overview of the ISPT program, describing the development status and technology infusion readiness of in-space propulsion technologies in the areas of electric propulsion, aerocapture, Earth entry vehicles, propulsion components, Mars ascent vehicle, and mission/systems analysis.
Document ID
20130000426
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Anderson, David J.
(NASA Glenn Research Center Cleveland, OH, United States)
Pencil,Eric J.
(NASA Glenn Research Center Cleveland, OH, United States)
Peterson, Todd
(NASA Glenn Research Center Cleveland, OH, United States)
Vento, Daniel
(NASA Glenn Research Center Cleveland, OH, United States)
Munk, Michelle M.
(NASA Langley Research Center Hampton, VA, United States)
Glaab, Louis J.
(NASA Langley Research Center Hampton, VA, United States)
Dankanich, John W.
(AeroDank, Inc. Cleveland, OH, United States)
Date Acquired
August 27, 2013
Publication Date
July 30, 2012
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-18519
Report Number: E-18519
Meeting Information
Meeting: 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2010
Location: Atlanta, GA
Country: United States
Start Date: July 30, 2012
End Date: August 1, 2012
Sponsors: American Society for Electrical Engineers, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 34620.01.13.01.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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