Publisher
American Institute of Aeronautics and Astronautics
Reference7 articles.
1. Bulman, M.J.,Aerojet-General Corporation, United States Patent US 6,568,171, "Rocket Vehicle Thrust Augmentation With Divergent Section of Nozzle," May 27, 2003.
2. Forde, S., Bulman, M., and Neill, T. " Thrust Augmentation Nozzle (TAN) Concept for Rocket engine Booster Applications", IAC-05-C4.3.03,56thInternational Astronautical Congress, Fukuoka, Japan, October17-21,2005.
3. Bulman, M.J., Messitt, D.G., Neill, T.M., and Borowski, S.K, "High Area Ratio LOX-Augmented Nuclear Thermal Rocket (LANTR) Testing", AIAA-2001-3369,37thAIAAJoint PropulsionConference, July 2001.
4. Mueggenburg, H.H., Hidahl, J.W., Kessler, E.L., Rousar, D.C. Platelet Actively Cooled Thermal Manage Devices" AIAA paper 92-3127,AIAA/SAE/ASME/ASEE 28th Joint Propulsion Conference, July 1992, Nashville, TN.
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