Experimental Study of Ballistic-Missile Base Heating with Operating Rocket
Description:
"A rocket of the 1000-pound-thrust class using liquid oxygen and JP-4 fuel as propellant was installed in the Lewis 8- by 6-foot tunnel to permit a controlled study of some of the factors affecting the heating of a rocket-missile base. Temperatures measured in the base region are presented from findings of three motor extension lengths relative to the base. Data are also presented for two combustion efficiency levels in the rocket motor" (p. 1).
Date:
September 23, 1958
Creator:
Nettles, J. Cary
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department