Liquid propulsion - Material compatibility
Compatibility during long term storage of liquid rocket propellants with spacecraft propulsion system materials
Engineering topics
Publications and source records attributed to Keller, O. F..
Compatibility during long term storage of liquid rocket propellants with spacecraft propulsion system materials
Bladder and expulsion devices for spacecraft liquid propulsion systems - pinhole leak test fixture, heat sterilization of ethylene propylene with hydrazine, and metal diaphragms
Diaphragm and balloon bladders for hydrazine expulsion in liquid propellant system and titanium tank fabrication
Advanced liquid propellants for spacecraft propulsion - nitrogen tetroxide and hydrazine
Gas flow is controlled by means of a pressure regulating system which prevents pressure surges. A high-pressure fluid source, a spring-loaded fluid-damped regulator valve, an accumulator, a conventional normally closed command valve, and a control valve are the main components.
Pressure regulating system with high pressure fluid source, adapted to maintain constant downstream pressure