Program Titan IIIM Standard Space Launch Vehicle Component Development Report for the Titan IIIM Stage 1 Combustion Chamber

Abstract

The increased thrust, higher engine performance, and greater reliability requirements of the Titan IIIM engines for application to the Manned Orbital Laboratory Program necessitated extensive redesign of the thrust chamber assembly as well as other major components for the Stage I engine. The report encompasses the design and development of the combustion chamber.

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Document Details

Document Type
Technical Report
Publication Date
Sep 05, 1969
Accession Number
AD0860050

Entities

People

  • W. J. Nord

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Human Systems
  • Weapons Technologies

DTIC Thesaurus Topics

  • Chemical Synthesis
  • Chemistry
  • Combustion Chambers
  • Computational Fluid Dynamics
  • Computer Programs
  • Control Systems
  • Fabrication
  • Finite Element Analysis
  • Heat Transfer
  • Materials
  • Measurement
  • Mechanical Working
  • Mechanics
  • Plastic Explosives
  • Strain Gages
  • Test And Evaluation
  • Test Stands

Fields of Study

  • Physics

Readers

  • Aerospace Engineering.
  • Combustion and Flow Dynamics.
  • Software Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster