Effect of ІІ stage propulsion system shut-down transients on launch vehicle performance capability
|1Shevchenko, BA, 1Nazarenko, EP, 1Ivanov, ОМ |
1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
|Kosm. nauka tehnol. 2005, 11 ;(Supplement1):021-023|
|Publication Language: Russian|
The article describes study of launch vehicle disturbances effect on hydraulic residual propellant during shut-down transients in propulsion system comprising main and vernier engines. The article is topical because of residual propellant effects significantly on launch vehicle performance capability.
1. Belyaev N. M. Calculation of pneumohydraulic missile systems, 224 p. (Mashinostroenie, Moscow, 1983) [in Russian]. 2. Belyaev N. M., Kalinichenko V. Ya., Shevchenko B. A. The effect of fluid oscillations on the height of the dip. Gas dynamics and elasticity theory. Numerical and analytical methods for solving problems of hydrodynamics and elasticity theory. Interuniversity collection of scientific papers. (DGU, Dnepropetrovsk, 1986) [in Russian]. 3. Polikovsky V. I., Perelman R. G. Vortex Funnel Formation in the Liquid with an Open Surface, 192 p. (Gosenergoizdat, Moscow, 1959) [in Russian]. 4. Ring E. Propulsion systems of rockets on liquid fuel, Transl. from Eng., 402 p. (Mir, Moscow, 1966) [in Russian].