BALLISTIC SUPPORT OF SPACECRAFT FLIGHT Russian patent published in 2015 - IPC B64G1/22 G01G17/04 

Abstract RU 2572003 C2

FIELD: transport.

SUBSTANCE: invention relates to spacecraft engineering and physics of gases and can be used for quantitative evaluation of the speed residual characteristic in the case of working medium reactive depletion in working system tanks. At initial and final stages of the working system operation working medium state equations are used to define the gas residual mass in the working system tanks.

EFFECT: ruled out accumulation of working medium residues determination errors.

2 dwg

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RU 2 572 003 C2

Authors

Afanas'Ev Sergej Mikhajlovich

Ankudinov Aleksandr Vladimirovich

Dates

2015-12-27Published

2013-09-17Filed