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,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1962-02-12

Pagination or Media Count:

88.0

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

Subject Categories:

  • Hydraulic and Pneumatic Equipment
  • Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE