Advanced Maneuvering Propulsion Technology Program.

Abstract

The engine design and analysis task was continued with completion of the secondary engine performance analysis, effort toward selecting the main engine thrust chamber segment support structure design, and effort toward completion of the main and secondary engine turbopump layout drawings. The engine critical component demonstration testing task was primarily directed toward completion of the full main thrust chamber fabrication and assembly. The major fabrication effort was completed, and assembly is in process. The oxidizer pump bearing and seal testing was continued. The main tester was damaged due to the suspected presence of solid contaminant, and the test program was continued with the secondary tester. The final Phase I analysis and design of the propellant feed system was completed by both General Dynamics/Convair and Lockheed Missiles and Space Company. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1970
Accession Number
AD0507273

Entities

Organizations

  • Rocketdyne

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Assembly
  • Chambers
  • Demonstrations
  • Dynamics
  • Engines
  • Environmental Pollutants
  • Fabrication
  • Propellants
  • Pumps
  • Thrust Chambers
  • Turbopumps

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Software Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster
  • Space - Satellites