Integrated NTP Vehicle Radiation Design

Caffrey, Jarvis A ; Rodriquez, Mitchell A

关键词: NUCLEAR PROPULSION;    RADIATION SHIELDING;    SPACECRAFT CABINS;    SPACECREWS;    THRUST-WEIGHT RATIO;    RADIATION HAZARDS;    MARS MISSIONS;    RISK;    EMITTANCE;    NUCLEAR REACTORS;    RADIATION DOSAGE;   

RP-ID  :  M18-6547

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

The 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.