PAPERS : DYNAMIC SIMULATION OF MISSILE BOOSTER SEPARATION |
Kim,Gu
Ji,Hyo-Seon |
1 | Richard E. Kreeger and Neil R. Walker, 'Supersonic Axial Stage Separation of an Unguided Rocket,' AIAA conference paper, 1997 |
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 |