Evaluation Test Report of Dynamic Characteristics of Derivative Pressure Feedback Type Servo Cylinders, GD/A-27-08550-11, GD/A-27-85314-815,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 12, 1962
- Accession Number
- AD0851622
Entities
People
- Charles B. Brantley
Organizations
- General Dynamics