Accession Number : AD0851313

Title :   Critical Engine Components Minimum Temperature Study Missile 36D,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Ramsay, D. L.

Report Date : 20 MAY 1960

Pagination or Media Count : 44

Abstract : The report presents the results of a critical engine components minimum temperature study using Missile 36D.

Descriptors :   (*SURFACE TO SURFACE MISSILES, LIQUID PROPELLANT ROCKET ENGINES), (*ENGINE COMPONENTS, THERMAL ANALYSIS), HEAT TRANSFER, CAPTIVE TESTS, PROPELLANT TRANSFER, LUBRICANTS, ELECTRIC SWITCHES, CONTROL SYSTEMS.

Subject Categories : Thermodynamics
      Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE