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Accession Number:
AD0804097
Title:
HYDRAULIC PLUMBING FOR ADVANCED AEROSPACE VEHICLES.
Corporate Author:
NORTH AMERICAN AVIATION INC LOS ANGELES CA LOS ANGELES DIV
Report Date:
1966-10-12
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.
Descriptive Note:
Quarterly technical rept. no. 1, 1 Jul-30 Sep 66.
Pages:
0041
Contract Number:
AF 33(615)-5407
File Size:
0.00MB
