Accession Number : AD0833374

Title :   EVALUATION OF ERECTION MECHANISM SPEED REDUCER,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Hendrickson, Stanley B.

Report Date : 25 AUG 1959

Pagination or Media Count : 9

Abstract : The object of this test was to determine the effect of temperature upon the performance of the missile erection speed reducer and to structurally proof-load the reducer at high, low and ambient temperatures. (Author)

Descriptors :   (*GUIDED MISSILE LAUNCHERS, POSITIONING DEVICES(MACHINERY)), (*REDUCTION GEARS, PERFORMANCE(ENGINEERING)), CONTROL SYSTEMS, PERFORMANCE(ENGINEERING), THERMAL STRESSES, LOADS(FORCES), TEMPERATURE, TORQUE, FRICTION, LUBRICANTS, VISCOSITY, BEARINGS.

Subject Categories : Construction Equipment, Materials & Supplies
      Machinery and Tools
      Guided Missile Launching and Basing Support

Distribution Statement : APPROVED FOR PUBLIC RELEASE