Funder
National Research Foundation of Korea
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Reference15 articles.
1. Unmack KE (1987) Wide range thrust throttling of a solid rocket motor. In: AIAA/SAE/ASME/ASEE 23rd joint propulsion conference, AIAA Paper No 1987-2085, June–July 1987
2. Kent SR, Loh TH, Chwalowski P (1995) Analytical contouring of pintle nozzle exit cone using computational fluid dynamics. In: 31st AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, AIAA Paper 1995-2877, July 1995.
https://doi.org/10.2514/6.1995-2877
3. Burroughs S (2001) Status of army pintle technology for controllable thrust propulsion. In: 37th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit, AIAA Paper 2001-3598, July 2001.
https://doi.org/10.2514/6.2001-3598
4. Sun P, Zhao X, Gao J (2013) Influencing analysis to nozzle’s inner flow field of different pintle radius and shapes. J Appl Sci 13(14):2744–2751.
https://doi.org/10.3923/jas.2013.2744.2751
5. Kim JG (2011) Study on the effects of pintle shapes and position in nozzle flow field, and thrust in a solid rocket motor with pintle nozzle. Ph.D. dissertation, Dept. of Mechanical Design Engineering, Chungnam National Univ., Daejeon, ROK
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