Accession Number:

AD0501962

Title:

Advanced Maneuvering Propulsion Technology Program.

Descriptive Note:

Quarterly progress rept. no. 6, 1 Feb-30 Apr 69.

Corporate Author:

ROCKETDYNE CANOGA PARK CALIF

Personal Author(s):

Report Date:

1969-06-01

Pagination or Media Count:

391.0

Abstract:

Analysis and design effort on the Advanced Maneuvering Propulsion System AMPS progressed satisfactorily during the sixth quarterly period. Engine critical component demonstration testing continued on the main thrust chamber segment hardware. A total of 19 firing tests were conducted on the 30-degree, hydrogen-cooled, channel-wall segments. Testing was initiated on the main fluorine pump bearings and seals. The basic analysis and design of the propellant feed system was completed by both General DynamicsConvair and Lockheed Missiles and Space Company. Author

Subject Categories:

  • Rocket Engines
  • Liquid Propellant Rocket Engines
  • Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE