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Enabling Deep Space Science Missions with Nuclear Thermal PropulsionNuclear thermal propulsion (NTP) enables entirely new classes of deep-space science missions to yield scientific returns that, in most cases, are simply not possible with traditional architectures. NTP systems can yield dramatically reduced interplanetary travel times, deliver roughly 2- 3 times (or more) the mass that can be delivered by conventional chemical propulsion systems, or provide a combination of these advantages to further enhance scientific return. Present NASA and DoD-sponsored plans for NTP systems will mature the technology using prototype and flight demonstration engines to prove the designs. These prototype engines will have performance in the correct thrust range so as to permit use as a low-risk propulsion stage in support of high-payoff deep space science missions. Additionally, the use of low-enriched Uranium (LEU) fuels over highly-enriched Uranium (HEU) fuels reduce the costs of engine development, qualification, acceptance and launch, and lowers the risks associated with proliferation management.
Document ID
20205004282
Acquisition Source
Marshall Space Flight Center
Document Type
White Paper
Authors
Kurt A Polzin
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
C Russell Joyner
(Aerojet Rocketdyne Rancho Cordova, California, United States)
Timothy Kokan
(Aerojet Rocketdyne Rancho Cordova, California, United States)
Stephen Edwards
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Adam Irvine
(Jacobs Huntsville, AL)
Mitchell Rodriguez
(Jacobs Huntsville, AL)
Michael Houts
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
July 9, 2020
Publication Date
July 15, 2020
Publication Information
Publication: White Paper
Publisher: Response to the Planetary Science and Astrobiology Decadal Survey 2023–2032 Call
Subject Category
Spacecraft Propulsion And Power
Funding Number(s)
WBS: 039889.01.01.62
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Professional Review
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