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

R.V. Bodnarchuk; A.A. Negoda; A..V. Novikov

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

Heading:

Space-Rocket Complexes

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

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

Full text (PDF)

References:

1. Polljak Ju. G. Probabilistic computer modeling, 256 p. (Sov. radio, Moscow, 1971) [in Russian].

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