Accession Number : AD0830625

Title :   THE VARIATION OF HEATING RATES IN A 1/30 SCALE BOOSTER ROCKET EXHAUST JET,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Sergeant, R. J.

Report Date : 28 AUG 1958

Pagination or Media Count : 23

Abstract : The report presents the test results pertaining to the heating rates encountered in the exhaust jet of a 1/30 scale booster rocket engine. (Author)

Descriptors :   *EXHAUST FLAMES), *THERMAL STRESSES), (*LIQUID PROPELLANT ROCKET ENGINES, (*GUIDED MISSILE LAUNCHERS, LAUNCH VEHICLES, MODEL TESTS, TEST METHODS, HEAT TRANSFER, THERMAL INSULATION, AERODYNAMIC HEATING, THERMOCOUPLES, MATHEMATICAL ANALYSIS, SCALE.

Subject Categories : Guided Missile Launching and Basing Support
      Surface-launched Guided Missiles
      Mechanics
      Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE