Accession Number : AD0842156

Title :   SCALE ATLAS VERNIER ROCKET FLAME EXPANSION STUDIES,

Corporate Author : GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

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

Report Date : 30 JUN 1960

Pagination or Media Count : 28

Abstract : This report describes test procedures for determining the possibility of vernier motor exhaust impingement heating. A one-tenth scale model rocket and an altitude chamber were utilized.

Descriptors :   *FLAME PROPAGATION), (*SURFACE TO SURFACE MISSILES, VERNIER ROCKET ENGINES), (*ROCKET NOZZLES, HIGH ALTITUDE, SIMULATION, GUIDED MISSILE MODELS, EXHAUST FLAMES, STABILIZATION, SHOCK WAVES, THERMAL RADIATION, COMPRESSIBLE FLOW.

Subject Categories : Surface-launched Guided Missiles
      Combustion and Ignition
      Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE