Concurrent rocket engine pre-conditioning and tank filling is disclosed. A disclosed example apparatus includes an inlet valve to supply a rocket propellant tank that is associated with a rocket engine with rocket propellant, and a flow director to direct at least a portion of a flow of the rocket propellant from the inlet valve to a chill line of the rocket engine to thermally condition the rocket engine as the rocket propellant tank is being filled with the rocket propellant.
CONCURRENT ROCKET ENGINE PRE-CONDITIONING AND TANK LOADING
2020-04-09
Patent
Elektronische Ressource
Englisch
Concurrent rocket engine pre-conditioning and tank loading
Europäisches Patentamt | 2022
|ROCKET PROPELLANT TANK ARRANGEMENT, ROCKET PROPULSION UNIT, AND ROCKET
Europäisches Patentamt | 2019
|Rocket propellant tank arrangement, rocket propulsion unit, and rocket
Europäisches Patentamt | 2024
|ROCKET ENGINE, ROCKET, AND METHOD FOR STARTING ROCKET ENGINE
Europäisches Patentamt | 2016
|ROCKET ENGINE, ROCKET, AND METHOD FOR STARTING ROCKET ENGINE
Europäisches Patentamt | 2015
|