The performance of Nuclear Electric Propulsion (NEP) in transporting cargo and propellant from Low Earth Orbit (LEO) to the first Earth-Moon Lagrange point (EML1) is examined. The baseline NEP vehicle utilizes a fission reactor system with Brayton power conversion for electric power generation to power multiple liquid hydrogen magnetoplasmadynamic (MPD) thrusters. Vehicle characteristics and performance levels are based on technology availability in a fifteen to twenty year timeframe. Results of numerical trajectory analyses are also provided.
High Power Nuclear Electric Propulsion (NEP) for Cargo and Propellant Transfer Missions in Cislunar Space
Space Technology and Applications International Forum (STAIF-2003) ; 2003 ; Albuquerque, NM, United States
2003-07-01
Report
Keine Angabe
Englisch
British Library Conference Proceedings | 2003
|Electric propulsion for cislunar missions
Engineering Index Backfile | 1966
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