MIL-S-18471 Revision G:1983
Current
The latest, up-to-date edition.
System, Aircrew Automated Escape, Ejection Seat Type, General Specification For
06-08-1983
Details requirements for the design, installation, (performance), demonstration, and testing of and open type escape system, which includes the ejection seat assembly, the aircraft canopy and escape path clearance subsystem, the sequencing subsystem, aircraft interface, and aircrew member interface.
DevelopmentNote |
INACTIVE FOR NEW DESIGN 18/9/96
|
DocumentType |
Standard
|
Pages |
115
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Current
|
This specification establishes the requirements for the design, installation, demonstration, performance, and testing of an open type ejection seat aircrew automated escape systems.
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