Experimental results of determining aerodynamic satellite characteristics in free-molecule gas flow

1Shabokhin, VA
1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 1998, 4 ;(1):68–70
Section: Spacecraft Dynamics and Control
Publication Language: Russian
We give some results of the  determination of aerodynamic drag coefficient from experimental data on satellite deceleration.
Keywords: erodynamic characteristics, spacecraft control
1. Bushuev E. I., Shabokhin V. A. Determination of the characteristics of interaction of a free molecular flow with a satellite surface. Kosmicheskie Issledovaniia na Ukraine, Is. 13, 32—36 (1979) [In Russian].
2. Bushuev E. I., Vasileva A. I., Kameko V. F., et al. Investigation of upper atmospheric density and satellite aerodynamics on the basis of orbital evolution data. In: Determination of spacecraft motion, 168—182 (Nauka, Moscow, 1975) [In Russian].
3. Omelik A. I. Experimental modeling in the free-molecular regime. In: Applied  Aerodynamics of Spacecraft, 40—49 (Naukova Dumka, Kiev, 1977) [in Russian].