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IGNITION SYSTEMS FOR ROCKET AND GUIDED MISSILE MOTORS. SAFETY DESIGN REQUIREMENTS - ED 3

contributor authorNATO - North Atlantic Treaty Organization
date accessioned2017-09-04T15:30:44Z
date available2017-09-04T15:30:44Z
date copyright08/01/2011
date issued2011
identifier otherAWSWTEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/32168
description abstractAIM
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).
languageEnglish
titleNATO STANAG 4368num
titleIGNITION SYSTEMS FOR ROCKET AND GUIDED MISSILE MOTORS. SAFETY DESIGN REQUIREMENTS - ED 3en
typestandard
page34
statusActive
treeNATO - North Atlantic Treaty Organization:;2011
contenttypefulltext


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