Advanced Maneuvering Propulsion Technology Program.
Quarterly progress rept. no. 5, 1 Nov 68-31 Jan 69.
ROCKETDYNE CANOGA PARK CALIF
Pagination or Media Count:
Engine critical component demonstration testing continued on the main thrust chamber segment hardware. A total of 28 tests was accomplished on the 30-degree tubular-wall segment thrust chamber, and 6 tests were accomplished on the 5-inch solid-wall segment thrust chamber which was modified to shorten its combustion chamber length. Preparations continued for testing of the bearings and seals for the LF2 pumps.
- Combustion and Ignition
- Rocket Engines
- Liquid Propellant Rocket Engines
- Liquid Rocket Propellants