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NTAC Augmented Nuclear and Advanced PropulsionCurrently, there are two types of nuclear propulsion: Nuclear Thermal Propulsion (NTP) and Nuclear Electric Propulsion (NEP). Common to both types, a nuclear reactor generates heat energy to raise the temperature of propellant, or the generated heat energy is converted into electric power. The electricity generated powers propulsion systems, such as a Hall thruster, magnetoplasma dynamic (MPD) thruster, or variable specific impulse magnetoplasma rocket (VASIMR). Customarily, only the thermal energy output from nuclear reaction is considered for NTP and NEP systems. However, the nuclear fission reaction can also generate ~7 MeV of prompt gamma rays. Therefore, most designers of NTP and NEP systems incorporate safety features to shield against this radiation. An optimized design approach would be to integrate a Nuclear Thermionic Avalanche Cell (NTAC) within the NTP or NEP structure for converting this radiation energy into additional electric power, while also shielding gamma rays. Consequently, this study addresses several combinations of NTP and NEP structures with NTAC devices in order to achieve that goal.
Document ID
20210024712
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Sang H Choi
(Langley Research Center Hampton, Virginia, United States)
Dennis M Bushnell
(Langley Research Center Hampton, Virginia, United States)
Robert W Moses
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
November 22, 2021
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: AIAA SciTech Forum
Location: San Diego, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 981698.01.03.23.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
[SG Notes: prov patent application filed February 25, 2021, LegalFiles indicates a non-provisional patent application is being prepared.]
Patent Application
Technical Review
Single Expert
Keywords
NTAC
NEP
NTP
Propulsion
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