Accession Number:

AD0804097

Title:

HYDRAULIC PLUMBING FOR ADVANCED AEROSPACE VEHICLES.

Descriptive Note:

Quarterly technical rept. no. 1, 1 Jul-30 Sep 66.

Corporate Author:

NORTH AMERICAN AVIATION INC LOS ANGELES CA LOS ANGELES DIV

Personal Author(s):

Report Date:

1966-10-12

Pagination or Media Count:

41.0

Abstract:

This program is an investigation of Hydraulic Plumbing for Advanced Aerospace Vehicles. The system is designed for 4,000 psi operating pressure with a fluit temperature range of -65 F to 500 F. The program is divided into 3 phases which are Phase I - The determination of hypothetical high performance air vehicle requirements, the procurement of tubing, and the design and selection of fittings for test. Phase II - The test of system components to provide basic data and fabrication techniques for installation of titanium plumbing in an air vehicle. Phase III - The installation of titanium plumbing in a simulator and simulator test.

Subject Categories:

  • Hydraulic and Pneumatic Equipment

Distribution Statement:

APPROVED FOR PUBLIC RELEASE