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Accession Number:
AD0860143
Title:
Aerodynamic Heating and Cooling Temperature Criteria Determination for Air-Launched Liquid Rocket Motors
Corporate Author:
NAVAL WEAPONS CENTER CHINA LAKE CA
Report Date:
1969-08-01
Abstract:
The thermal regime of a 12-inch diameter liquid rocket motor, while carried by F4B and A6A aircraft, is investigated. Aerodynamic heating is measured during carriage by the F4B aircraft. Aerodynamic cooling is investigated during flights of up to 4 12 hours on A6A aircraft. The report includes figures which give the heating and cooling profiles, and tables.
Descriptive Note:
Technical publication
Pages:
0047
Distribution Statement:
Approved for public release; distribution is unlimited.
File Size:
1.35MB
