References
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- 'Aerodynamic Characteristics of The Pershing Missile during Separation of Its Three Stage', NASA TM SX-524
- Drakin, N. I., 'Aerodynamic Ray Heating in Flight', 러시아 문헌, 국방과학연구소 소장
- 로켓 공력 설계 자료, 중국문헌, 국방과학연구소 소장
- Walker, R. E., Stone, A. R., and Shandor, M., 'Secondary Gas Injection in a Conicial Rocket Nozzle,' AIAA Journal, Feb. 1963
Cited by
- A Study of Numerical Analysis for Stage Separation Behavior of Two-body Vehicle vol.22, pp.4, 2018, https://doi.org/10.6108/KSPE.2018.22.4.091