Advanced Maneuvering Propulsion Technology Program.

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.

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1969
Accession Number
AD0395932

Entities

Organizations

  • Rocketdyne

Tags

DTIC Thesaurus Topics

  • Burnthrough
  • Chambers
  • Chemical Reactions
  • Combustion
  • Combustion Chambers
  • Demonstrations
  • Engines
  • Exothermic Reactions
  • Heat Engines
  • Heat Transfer Devices
  • Ignition
  • Ignition Lag
  • Thrust Chambers

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Software Engineering