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
Distribution Statement : APPROVED FOR PUBLIC RELEASE