MIL-S-18471G(AS)
8 June 1983
SUPERSEDING
MIL-S-18471F(AS)
13 October 1978
MILITARY SPECIFICATION
SYSTEM, AIRCREW AUTOMATED ESCAPE, EJECTION SEAT TYPE:
GENERAL SPECIFICATION FOR
This specification is approved for use by the Naval Air
Systems Command, Department of the Navy and is available for
use by all Departments and Agencies of the Department of Defense.
SCOPE
1.
1.1 Scope. This specification establishes the requirements for the
design, installation, demonstration, performance, and testing of an open type
ejection seat aircrew automated escape systems. The escape system includes
the ejection seat assembly, the aircraft canopy and escape path clearance
subsystem the sequencing subsystem aircraft interface and the aircrewmember
interface.
2.
APPLICABLE DOCUMENTS
2.1 Government documents
2.1.1 Specifications, standards, and handbooks. Unless otherwise spec-
ified, the following specifications, standards and handbooks of the issue
listed in that issue of the Department of Defense Index of Specifications
and Standards (DoDISS) specified in the solicitation form a part of this
specification to the extent specified herein.
SPECIFICATIONS
FEDERAL
Chromium Plating (Electrodeposited)
QQ-C-320
Plating, Cadmium (Electrodeposited)
QQ-P-416
Boxes, Wood, Cleated Plywood
PPP-B-601
Cushioning Materials, Flexible, Cellular,
PPP-C-795
Plastic Film For Packaging Applications
Beneficial comments (recommendations, additions, deletions) and any pertinent
data which may be of use in improving this document should be addressed to:
the Commanding Officer, Naval Air Engineering Center, Engineering Specifica-
tions and Standards Department (ESSD), Code 93, Lakehurst, NJ 08733 by using
the self-addressed Standardization Document Improvement Proposal (DD Form .
1426) appearing at the end of this document or by letter.
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