Mars NTP Architecture Elements Using the Lunar Orbital Platform-Gateway
Author:
Affiliation:
1. Aerojet Rocketdyne
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5105
Reference5 articles.
1. 4Venneri, P. F., Kim, Y. "A FeasibilityStudyon Low-Enriched UraniumFuel for Nuclear Thermal Rockets-II: Rocket and ReactorPerformance,"Progress inNuclear Energy, Volume83, August 2015,Pages406-418.
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