MIL-STD-1901A
FOREWORD
1. This Military Standard is approved for use by all Departments and Agencies of the
Department of Defense.
2. 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.
3. 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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