An engine start system includes a facility that has a ground based hydraulic pressurization system and a combustor of a liquid propellant rocket engine. The engine is fluidly coupled to the ground based hydraulic pressurization system. The liquid propellant rocket engine is operably detachable from the ground based hydraulic pressurization system.
GROUND HYDRAULIC SYSTEM HYPERGOLIC SLUG INJECTION
HYDRAULISCHES BODENSYSTEM MIT HYPERGOLISCHER SLUG-INJEKTION
SYSTÈME HYDRAULIQUE AU SOL AVEC INJECTION DE LINGOT HYPERGOLIQUE
2020-11-11
Patent
Electronic Resource
English