The Revolutionary Aerospace Systems Concepts (RASC) team, led by the NASA Langley Research Center, is tasked with exploring revolutionary new approaches to enabling NASA to achieve its strategic goals and objectives in future missions. This paper provides the details from the 2004–2005 RASC study of a point‐design that uses a high‐power nuclear electric propulsion (NEP) based space transportation architecture to support a manned mission to Mars. The study assumes a high‐temperature liquid‐metal cooled fission reactor with a Brayton power conversion system to generate the electrical power required by magnetoplasmadynamic (MPD) thrusters. The architecture includes a cargo vehicle with an NEP system providing 5 MW of electrical power and a crewed vehicle with an NEP system with two reactors providing a combined total of 10 MW of electrical power. Both vehicles use a low‐thrust, high‐efficiency (5000 sec specific impulse) MPD system to conduct a spiral‐out of the Earth gravity well, a low‐thrust heliocentric trajectory, and a spiral‐in at Mars with arrival late in 2033. The cargo vehicle carries two moon landers to Mars and arrives shortly before the crewed vehicle. The crewed vehicle and cargo vehicle rendezvous in Mars orbit and, over the course of the 60‐day stay, the crew conducts nine‐day excursions to Phobos and Deimos with the landers. The crewed vehicle then spirals out of Martian orbit and returns via a low‐thrust trajectory to conduct an Earth flyby. The crew separates from the vehicle prior to Earth flyby and aerobrakes for a direct‐entry landing.
Use of High‐Power Brayton Nuclear Electric Propulsion (NEP) for a 2033 Mars Round‐Trip Mission
SPACE TECH.& APPLIC.INT.FORUM-STAIF 2006: 10th Conf Thermophys Applic Microgravity; 23rd Symp Space Nucl Pwr & Propulsion; 4th Conf Human/Robotic Tech & Nat'l Vision for Space Explor.; 4th Symp Space Coloniz.; 3rd Symp on New Frontiers & Future Concepts ; 2006 ; Albuquerque, New Mexico (USA)
AIP Conference Proceedings ; 813 , 1 ; 222-229
2006-01-20
8 pages
Conference paper
Electronic Resource
English
Use of High-Power Brayton Nuclear Electric Propulsion (NEP) for a 2033 Mars Round-Trip Mission
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