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NATO - STANAG 3950

Helicopter Design Criteria for Crew Crash Protection and Anthropometric Accommodation

inactive
Organization: NATO
Publication Date: 14 February 2001
Status: inactive
Page Count: 39

Document History

STANAG 3950
February 14, 2001
Helicopter Design Criteria for Crew Crash Protection and Anthropometric Accommodation
AIM The aim of this agreement is to provide helicopter design criteria for crash protection and anthropometric accommodation of the crew.
STANAG 3950
February 14, 2001
Helicopter Design Criteria for Crew Crash Protection and Anthropometric Accommodation
A description is not available for this item.
STANAG 3950
January 1, 1991
Helicopter Crew Seat Design
A description is not available for this item.
STANAG 3950
January 1, 1991
Helicopter Crew Seat Design
A description is not available for this item.

References

This document references:
MIL-STD-1290 - LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
Published by NPFC on January 17, 2006
A description is not available for this item.
This document references:
ISO 2631-1 - Mechanical vibration and shock — Evaluation of human exposure to whole-body vibration — Part 1: General requirements AMENDMENT 1
Published by ISO on July 1, 2010
This part of ISO 2631 defines methods for the measurement of periodic, random and transient whole-body vibration. It indicates the principal factors that combine to determine the degree to which a...
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