NTP Design Derivatives and Enhancements for Lunar and Mars Missions
Author:
Affiliation:
1. Aerojet Rocketdyne
2. Ultra Safe Nuclear Corporation
Publisher
American Institute of Aeronautics and Astronautics
Reference16 articles.
1. Enabling Multiple Abort Strategies Using the NTP Approach for Human Mars Missions
Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Corrosion and microstructural characterization of molybdenum cermets following hydrogen exposure up to 2630K;Journal of Nuclear Materials;2023-12
2. In Situ Propellant Alternatives for a Lunar Ascent/Descent Vehicle;Journal of Spacecraft and Rockets;2023-09
3. Propulsion Alternatives for Mars Transportation Architectures;Journal of Spacecraft and Rockets;2023-03
4. Impacts of In Situ Alternative Propellant on Nuclear Thermal Propulsion Mars Vehicle Architectures;Journal of Spacecraft and Rockets;2022-11
5. Human Mars Mission Transit Abort Options for Ballistic High Thrust and Hybrid Transportation Systems;ASCEND 2022;2022-10-15
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