Patent · US Active

Supply system for supplying a rocket engine

US11371468B2 · kind B2 · utility

0Cited by
5References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 21, 2018
Grant dateJun 28, 2022
Priority date
Expiry dateAug 21, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/96
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A supply system for supplying a rocket engine with at least one propellant, the supply system comprising at least one supply circuit able to circulate the propellant, and at least one reservoir in fluid communication with the supply circuit via at least one communication pipe, so that a fluid contained in the reservoir can flow from the latter up to the supply circuit, and vice versa, via said at least one communication pipe, the reservoir being able to contain a volume of gas, and heating means able to vary the volume of gas in the reservoir, the heating means being configured to vaporize the propellant in the reservoir.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.