Author:
Forde Scott,Bulman Mel,Neill Todd
Reference7 articles.
1. M.J. Bulman, Aerojet-General Corporation, United States Patent US 6,568,171, Rocket vehicle thrust augmentation with divergent section of nozzle, May 27, 2003.
2. S.K. Borowski, R.R. Corban, D.W. Culver, M.J. Bulman, M.C. McIlwain, A revolutionary lunar space transportation system architecture using extraterrestrial LOX-augmented NTR Propulsion, AIAA-94-3343, 30th AIAA Joint Propulsion Conference, July 1994.
3. M.J. Bulman, D.G. Messitt, T.M. Neill, S.K. Borowski, High area ratio LOX-augmented nuclear thermal rocket (LANTR) testing, AIAA-2000-3897, 36th AIAA Joint Propulsion Conference, July 2000.
4. M.J. Bulman, D.G. Messitt, T.M. Neill, S.K. Borowski, High area ratio LOX-augmented nuclear thermal rocket (LANTR) testing, AIAA-2001-3369, 37th AIAA Joint Propulsion Conference, July 2001.
5. M.J. Bulman, D.G. Messitt, T.M. Neill, S.K. Borowski, Continued LOX-augmented nuclear thermal rocket (LANTR) testing, AIAA-2002-3650, 38th AIAA Joint Propulsion Conference, July 2002.
Cited by
10 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献