Titan IIIM Standard Space Launch Vehicle Development Report for the Stage I Engine Demonstration Testing

Abstract

The objective of the demonstration test program was to confirm the validity of the new component designs by engine tests at both nominal and extreme Titan IIIM operating conditions without unnecessarily repeating the Titan II and Titan III qualification tests. The test program also served as a convenient vehicle for testing related items, not intrinsic to the engine system, such as the Martin POGO accumulators, gimbal actuators, flight instrumentation, and ground equipment. The planned program consisted of 30 tests, 15 on each of two engines.

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Document Details

Document Type
Technical Report
Publication Date
Mar 31, 1969
Accession Number
AD0850432

Entities

People

  • L. D. Reber

Organizations

  • Aerojet Rocketdyne Holdings

Tags

Communities of Interest

  • Air Platforms
  • Ground and Sea Platforms
  • Human Systems
  • Sensors
  • Weapons Technologies

DTIC Thesaurus Topics

  • Assembly
  • Chemical Synthesis
  • Combustion Chambers
  • Detection
  • Engine Components
  • Fabrication
  • Heat Transfer
  • Manufacturing
  • Material Degradation Processes
  • Materials
  • Materials Processing
  • Materials Science
  • Measurement
  • Plastic Explosives
  • Self Assembly
  • Spacers
  • Test And Evaluation

Readers

  • Aerospace Engineering.
  • Control Systems Engineering.
  • Software Engineering

Technology Areas

  • Space