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MIL-STD-1901A: Munition Rocket and Missile Motor Ignition System Design, Safety Criteri |
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FOREWORD
FOREWORD
- This Military Standard is approved for use by all
Departments and Agencies of the Department of Defense.
- The purpose of this standard is to establish specific
design safety criteria for Ignition Systems and Ignition Safety Devices
intended for use with munition rockets and missile motors. The safety,
arming, and firing requirements specified herein are mandatory fundamental
elements of engineering design, development, and testing. Ignition systems
shall provide primary safety for propulsion systems consistent with
assembly, handling, storage, transportation, operational readiness, and use
or disposal. The inadvertent actuation of a munition propulsion system can
result in catastrophic material damage and injury or death to personnel.
Every effort must be made during the development of munition propulsion
systems with their associated initiation systems, to achieve a high degree
of safety through the incorporation of good design features and the
selection and use of materials and operating procedures. The thrust toward
in-field testing of powered weapons further increases the exposure of
operating personnel to the threat of inadvertent actuation of the munition
propulsion system.
- Beneficial comments (recommendations, additions, deletions)
and any pertinent data which may be of use in improving this document shall
be addressed to: Commander, US Army TACOM-ARDEC, ATTN: AMSTA-AR-QAW-E,
Picatinny Arsenal, NJ 07806-5000 by using the self-addressed Standardization
Document Improvement Proposal (DD Form 1426) appearing at the end of this
document or by letter. Comments should be forwarded through the designated
Reviewing Activity listed for each Service in
4.14.
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