DocumentCode
158373
Title
The status of spacecraft bus and platform technology development under the NASA ISPT program
Author
Anderson, D.J. ; Munk, M.M. ; Pencil, E. ; Dankanich, J. ; Glaab, L. ; Peterson, T.
Author_Institution
NASA Glenn Res. Center, Cleveland, OH, USA
fYear
2014
fDate
1-8 March 2014
Firstpage
1
Lastpage
18
Abstract
The 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. ISPT´s propulsion technologies include: 1) NASA´s 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. ISPT´s 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 (GN&C) 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 pa- er provides a brief overview of the ISPT program, describing the development status and technology infusion readiness.
Keywords
aerospace engines; aerospace instrumentation; aerospace propulsion; aerospace testing; electric propulsion; ion engines; Earth entry vehicles; Hall-effect electric propulsion system; Mars Ascent Vehicle; NASA Evolutionary Xenon Thruster; NASA ISPT Program; NASA robotic science missions; NEXT ion propulsion system; advanced xenon flow control system; entry vehicle technologies; in-space propulsion technologies; multimission technologies; platform technology; propulsion system technologies; spacecraft bus; systems-mission analysis; throttle-able gridded ion system; ultralightweight propellant tank technologies; Investment; NASA; Pollution measurement; Propulsion; Space vehicles; Xenon;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2014 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
978-1-4799-5582-4
Type
conf
DOI
10.1109/AERO.2014.6836363
Filename
6836363
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