Investigation of some features of flight dynamics and the cause of scattering of launching-vehicle separating parts

1Bodnarchuk, RV, 2Negoda, AA, 3Novikov, AV
1Regional Branch of the National Institute for Strategic Studies, Dnipropetrovsk, Ukraine
2State Space Agency of Ukraine, Kyiv, Ukraine
3Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 1995, 1 ;(2):55–59
https://doi.org/10.15407/knit1995.02.055
Section: Space-Rocket Vehicles
Publication Language: Russian
Abstract: 
Topical problems in the dynamics of LV separating part (SP) descent in dense atmospheric layers are investigated by the statistical testing method. Special features of its angular oscillation, their influence on the flying range and on the mechanism of scattering of SP dropping points are also analysed
Keywords: launching-vehicle, scattering, separating parts
References: 
1. Polljak Ju.  G. Probabilistic computer modeling, 256 p. (Sov. radio, Moscow, 1971) [in Russian].