Simulating the efficiency of the means ensuring fuel continuity in space vehicles

1Makarova, AS, 1Davydov, SA, 1Sorokina, LA, 1Davydova, AV
1Oles Honchar National University of Dnipropetrovsk, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 1998, 4 ;(2):117–118
https://doi.org/10.15407/knit1998.02.117
Section: Space Energy, Power and Propulsion
Publication Language: Russian
Abstract: 
We propose calculation procedures for determining the holding capacity of the means that ensure fuel continuity in space vehicles under the dynamic impulsive or vibrational load as well as at transition stages of power-plant operation.
Keywords: ensure fuel continuity in space vehicles, simulating, space power
References: 
1. Gluck D. F. Propellant position control by capillari barriers during spacecraft rotational maneuvers. AIAA paper, N 529, 8 p. (1969).
2. Tegart J. R. Influens of pressure transients on the perfomance of capillary propellant acquisition system. AIAA paper, N 597, 8 p. (1976).