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.
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