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NATO - STANAG 4368

IGNITION SYSTEMS FOR ROCKET AND GUIDED MISSILE MOTORS. SAFETY DESIGN REQUIREMENTS

active, Most Current
Organization: NATO
Publication Date: 1 August 2011
Status: active
Page Count: 34
scope:

AIM

The aim of this agreement is to standardize the safety design requirements for ignition systems for rocket and guided missile solid propellant motors used in non-nuclear systems. These safety requirements may be applied to ignition systems of other types of motors, as deemed applicable by the National Safety Approving Authorities (NSAA).

Document History

STANAG 4368
August 1, 2011
IGNITION SYSTEMS FOR ROCKET AND GUIDED MISSILE MOTORS. SAFETY DESIGN REQUIREMENTS
AIM The aim of this agreement is to standardize the safety design requirements for ignition systems for rocket and guided missile solid propellant motors used in non-nuclear systems. These safety...
February 25, 2002
Electric and Laser Ignition Systems for Rockets and Guided Missile Motors Safety Design Requirements
AIM The aim of this agreement is to standardise the design safety requirements for electrical and laser ignition systems for rockets and guided missile motors used in non-nuclear weapon systems.
February 16, 1998
Electric and Laser Ignition Systems for Rockets and Guided Missile Motors - Safety Design Requirements
A description is not available for this item.

References

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