Technical Paper
Design and Fabrication of Small H2/O2 Engines
1970-02-01
700803
Hydrogen/oxygen propulsion systems with thrust levels in the order of 1500 pounds are being studied for future space vehicle auxiliary propulsion systems. ...Hydrogen/oxygen propulsion systems with thrust levels in the order of 1500 pounds are being studied for future space vehicle auxiliary propulsion systems. Because of the 10-year reusable requirement for these types of missions, thrust chamber designs must provide long life capability.
