Accession Number : AD0851622

Title :   Evaluation Test Report of Dynamic Characteristics of Derivative Pressure Feedback Type Servo Cylinders, GD/A-27-08550-11, GD/A-27-85314-815,

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Brantley, Charles B.

Report Date : 12 FEB 1962

Pagination or Media Count : 88

Abstract : Because of the increased load on the Atlas created by the Centaur upper stage and the increase in over-all length of the two and a half stage missile, a program was initiated in order to decrease the dynamic load on the missile. (Author)

Descriptors :   (*LAUNCH VEHICLES, HYDRAULIC SERVOMECHANISMS), (*HYDRAULIC SERVOMECHANISMS, PERFORMANCE(ENGINEERING)), HYDRAULIC EQUIPMENT, ORIFICES, RESPONSE, LOADS(FORCES), PRESSURE, FEEDBACK, HYSTERESIS, PHASE SHIFT CIRCUITS.

Subject Categories : Hydraulic and Pneumatic Equipment
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE