Spacecraft Bus and Platform Technology Development under the NASA ISPT Program
Spacecraft Bus and Platform Technology Development under the NASA ISPT Program
- New search for: Anderson, David J.
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- New search for: Dankanich, John W.
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- New search for: Anderson, David J.
- New search for: Munk, Michelle M.
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- New search for: Dankanich, John W.
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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 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 near-term flight infusion: 1) the high-temperature Advanced Material Bipropellant Rocket (AMBR) engine providing higher performance 2) NASAs 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 being developed with flight infusion in mind are the Advanced Xenon Flow Control System, and ultra-lightweight propellant tank technologies. Future direction for ISPT are technologies that relate to sample return missions and other spacecraft bus technology needs 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 and mission-focused, and present a different set of technology development and infusion steps beyond those previously implemented. The Systems/Mission Analysis area is focused on developing tools and assessing the application of propulsion and spacecraft bus 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 information
Spacecraft Bus and Platform Technology Development under the NASA ISPT Program
JANNAF Modeling and Simulation (MSS) Joint Subcommittee meeting
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2013
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Colorado Springs, CO, United States
JANNAF Spacecraft Propulsion Joint Subcommittee meeting
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2013
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Colorado Springs, CO, United States
JANNAF Liquid Propulsion (LPS) Joint Subcommittee meeting
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2013
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Colorado Springs, CO, United States
JANNAF Joint Interagency Propulsion Committee meeting
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2013
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Colorado Springs, CO, United States
2013-04-29
Conference paper
No indication
English