| 摘要 |
A method for pressurization of fuel tanks of propulsion systems of carrier rockets includes storing working fluid of pressurization on a rocket board, its heating in flight in a heat exchanger of a propulsion system and supply into the free volume of the fuel tank by a pressurization line. Before starting the propulsion system the heat exchanger of the propulsion system and pressurization line are heated to the temperatures allowable by strength requirements. |
