Affordable Development and Qualification Strategy for Nuclear Thermal Propulsion
Author:
Affiliation:
1. NASA Marshall Space Flight Center
2. RENMAR Enterprises, Inc.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4161
Reference21 articles.
1. A Rational Strategy for Nuclear Thermal Rocket Development
2. 3Altseimer, J. H., Mader, G. F., Stewart, J. J. "Operating Characteristics and Requirements for the NERVA Flight Engine," Paper 70-676, AIAA6thPropulsionJointSpecialistConference,June1970.
3. 4Drake,B.G."HumanMarsMissionDefinition:Requirements&Issues,"presentation,Human2MarsSummit,May2013.
4. 5"NASA's huge new rocket may cost $500 million per launch". http://www.nbcnews.com/id/49019843/ns/technology_and_science-space/#.UcHSyXewV8G ,MSNBC. September 12,2012.
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