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http://dx.doi.org/10.5139/JKSAS.2004.32.1.058

PAPERS : DYNAMIC SIMULATION OF MISSILE BOOSTER SEPARATION  

Kim,Gu
Ji,Hyo-Seon
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.32, no.1, 2004 , pp. 58-64 More about this Journal
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  • Reference
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2 'Aerodynamic Characteristics of The Pershing Missile during Separation of Its Three Stage', NASA TM SX-524
3 Drakin, N. I., 'Aerodynamic Ray Heating in Flight', 러시아 문헌, 국방과학연구소 소장
4 로켓 공력 설계 자료, 중국문헌, 국방과학연구소 소장
5 Walker, R. E., Stone, A. R., and Shandor, M., 'Secondary Gas Injection in a Conicial Rocket Nozzle,' AIAA Journal, Feb. 1963