Accession Number : AD0893261

Title :   Aerocooling of a 12-Inch Diameter Missile During Air Carry.

Descriptive Note : Technical publication,

Corporate Author : NAVAL WEAPONS CENTER CHINA LAKE CA

Personal Author(s) : Schafer, H. C.

Report Date : FEB 1972

Pagination or Media Count : 62

Abstract : A series of flights using A6A aircraft and the small Bullpup airframe were made at 40,000, 30,000 and 20,000 feet. The resulting continuous time-temperature records of the JP-4 and JP-5 filled motor section are presented. The guidance and control section thermal response is also presented. Flight parameters included meteorological air temperatures of -78F for 2 1/2 hours exposure time. (Author)

Descriptors :   (*JET ENGINE FUELS, THERMAL ANALYSIS), (*AIR TO SURFACE MISSILES, JET ENGINE FUELS), HIGH ALTITUDE, AIR COOLED, FLIGHT TESTING, ATMOSPHERIC TEMPERATURE, STATISTICAL DATA.

Subject Categories : Air- and Space-launched Guided Missiles
      Fuels

Distribution Statement : APPROVED FOR PUBLIC RELEASE