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Page Title:
Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation & Data Requirements for, General Specification For |
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|  MIL-H-8891A
23 January 1978
SUPERSEDING
MIL-H-8891
MILITARY SPECIFICATION
HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES, TYPE III
DESIGN, INSTALLATION & DATA REQUIREMENTS FOR,
GENERAL SPECIFICATION FOR
This specification is approved for use by all Departments
and Agencies of the Department of Defense.
1.
SCOPE
Scope - This specification covers the design and in-
1.1
stallation requirements for Type III manned flight vehicle hydraulic systems.
Classification - Type III flight vehicle hydraulic
1.2
0
o
systems for temperature range from -65 + 39 F (see 3.3) shall be of the
following classes, as specified:
Class 3,000 pound per square inch (psi) - Where the cutout pressure
at the main pressure controlling device is 3,000 psi.
Class 4,000 psi - Where the cutout pressure at the main pressure
controlling device is 4,000 psi.
2.
APPLICABLE DOCUMENTS
*
Issues of Documents - The following documents, of the
2.1
issue in effect on date of invitation for bids or request for proposal, form
a part of this specification to the extent specified herein:
SPECIFICATIONS
Military
MIL-B-5087
Bonding, Electrical, and Lighting Protection
for Aerospace Systems
Wiring, Aircraft, Installation of
MIL-W-5088
MIL-H-5440
Hydraulic Systems, Aircraft, Types I and II,
Design, Installation and Data Requirements for
*
Beneficial comments (recommendations, additions, deletions) and any
pertinent data which may be of use in improving this document should
be addressed to: Engineering Specifications and Standards Department
(Code 93) Naval Air Engineering Center, Lakehurst, N.J. 08733, by
using the self-addressed Standardization Document Improvement Proposal
(DD Form 1426) appearing at the end of this document or by letter.
FSC 1650
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