FIELD: rocket and space engineering.
SUBSTANCE: fuel tanks for propulsion systems of spacecraft. The fuel tank contains an outer casing, an equidistantly spaced shell with holes to form an intake cavity, and an elastic fuel displacer in the form of four containers exposed to excess gas pressure.
EFFECT: reduction in weight and size characteristics and an increase in the reliability of the functioning of the fuel tank and the propulsion system as a whole.
1 cl, 5 dwg
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|
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