Accession Number:

AD0829923

Title:

DESIGN SYNOPSIS AIRCRAFT HYDRAULIC SYSTEMS,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1952-01-05

Pagination or Media Count:

39.0

Abstract:

This design synopsis of aircraft hydraulic systems is intended to convey to designers computation data and information concerning applicable specifications. Design, installation and construction of the hydraulic systems in military aircraft is governed by Specification MIL-H-5440 Hydraulic Systems Design, Installation and Tests of Aircraft and a large number of detail specifications referenced therein. These specifications are not mandatory for commercial aircraft but the wise designer will use them unless they involve a severe weight or cost penalty. Author

Subject Categories:

  • Aircraft
  • Hydraulic and Pneumatic Equipment
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE