PARTIAL QUALIFICATION TEST OF TITAN I ENGINE COMPONENT THRUST CHAMBER ASSEMBLY CONTROLS, AEROJET-GENERAL CORPORATION, SACRAMENTO, CALIFORNIA

Abstract

Purpose of this program was to subject one assembly of the Titan I first stage thrust chamber controls to the flight simulation test phase of a qualification test program. A detailed description of the test program, along with the test equipment employed in the performance of the test program is included. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 15, 1961
Accession Number
AD0262455

Entities

People

  • L.n. Mortenson
  • R.b. Clark

Tags

DTIC Thesaurus Topics

  • Assembly
  • California
  • Chambers
  • Corporations
  • Engine Components
  • Engine Fuel Systems Components
  • Engines
  • Flight Simulations
  • Qualifications
  • Simulations
  • Simulators
  • Test Equipment
  • Thrust Chambers

Fields of Study

  • Medicine
  • Physics

Readers

  • Logistics and Supply Chain Management.
  • Rocket Propulsion.