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Integrated NTP Vehicle Radiation DesignThe development of a nuclear thermal propulsion stage requires consideration for radiation emitted from the nuclear reactor core. Applying shielding mass is an effective mitigating solution, but a better alternative is to incorporate some mitigation strategies into the propulsion stage and crew habitat. In this way, the required additional mass is minimized and the mass that must be applied may in some cases be able to serve multiple purposes. Strategies for crew compartment shielding are discussed that reduce dose from both engine and cosmic sources, and in some cases may also serve to reduce life support risks by permitting abundant water reserves. Early consideration for integrated mitigation solutions in a crewed nuclear thermal propulsion (NTP) vehicle will enable reduced radiation burden from both cosmic and nuclear sources, improved thrust-to-weight ratio or payload capacity by reducing 'dead mass' of shielding, and generally support a more robust risk posture for a NTP-powered Mars mission by permitting shorter trip times and increased water reserves.
Document ID
20180002056
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Caffrey, Jarvis A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rodriquez, Mitchell A.
(Jacobs Technology, Inc. Huntsville, AL, United States)
Date Acquired
March 22, 2018
Publication Date
February 26, 2018
Subject Category
Space Radiation
Spacecraft Propulsion And Power
Report/Patent Number
M18-6547
Meeting Information
Meeting: Nuclear and Emerging Technologies for Space (NETS) Conference
Location: Las Vegas, NV
Country: United States
Start Date: February 26, 2018
End Date: March 1, 2018
Sponsors: American Nuclear Society
Distribution Limits
Public
Copyright
Public Use Permitted.
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