Accession Number:

AD0395932

Title:

Advanced Maneuvering Propulsion Technology Program.

Descriptive Note:

Quarterly progress rept. no. 5, 1 Nov 68-31 Jan 69.

Corporate Author:

ROCKETDYNE CANOGA PARK CALIF

Personal Author(s):

Report Date:

1969-03-01

Pagination or Media Count:

493.0

Abstract:

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.

Subject Categories:

  • Combustion and Ignition
  • Rocket Engines
  • Liquid Propellant Rocket Engines
  • Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE