METHOD OF FILLING WITH LIQUID OXYGEN OF TANK OF CARRIER ROCKET OF AVIATION MISSILE SYSTEM

摘要

A method of filling with liquid oxygen of a tank of a carrier rocket of an aviation missile system includes filling with liquid oxygen of the tank of the carrier rocket to a predetermined level and with cryogenic component of a cryogenic tank, which are located in the cargo compartment of the aircraft, and temperature control of the liquid oxygen in the tank of carrier rocket during flight of an aircraft up to landing at a given height using a cryogenic tanks with cryogenic component circulating through the tank of carrier rocket, when connecting the gas part of the tank to atmosphere. As a cryogenic component in a cryogenic tank a liquid nitrogen is used with initial temperature corresponding to its boiling point at normal atmospheric pressure.