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Fuze Well Mechanical Interface

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AS5680B
  • Current
Published 2019-09-03 by SAE International in United States
This interface standard applies to fuzes used in airborne weapons that use a 3-in fuze well. It defines: Physical envelope of the fuze well at the interface with the fuze. Load bearing surfaces of the fuze well. Physical envelope of the fuze and its connector. Mechanical features (e.g., clocking feature). Connector type, size, location and orientation. Retaining ring and its mechanical features (e.g., thread, tool interface). Physical envelope of the retaining ring at the interface with the fuze. Physical space available for installation tools. Torque that the installation tool shall be capable of providing. This standard does not address: Materials used or their properties. Protective finish. Physical environment of the weapon. Explosive interface or features (e.g., insensitive munitions (IM) mitigation). Charging tube. Torque on the retaining ring or loads on the load bearing surfaces. Each fuze and weapon combination should be evaluated to ensure that the weapon system will satisfy all safety, reliability, and performance requirements throughout its lifecycle.
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Validation Methods for MIL-STD-1760C Aircraft Station Interfaces

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AS47642B
  • Current
Published 2017-06-28 by SAE International in United States
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760C. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies. For validation of aircraft designed to MIL-STD-1760B Notice 3 AS47641 Issued 1999-08 applies.
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Validation Methods for MIL-STD-1760B Aircraft Station Interfaces

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AS47641A
  • Current
Published 2017-06-28 by SAE International in United States
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760B Notice 3. For validation of aircraft designed to MIL-STD-1760A Notice 2 AS4764 Issued 1995-04 applies.
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Considerations for Safe Store Operation on Manned and Unmanned Vehicles

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AIR6027A
  • Current
Published 2017-06-27 by SAE International in United States
The information presented in this AIR is intended to provide designers of armed unmanned systems with guidelines that may be applied to ensure safe integration and operation of weapons on unmanned platforms. The guidelines have been developed from experiences gained in the design and operation of weapons on manned aircraft that have been accepted by relevant safety authorities in the USA and Europe and proven effective over many years. Whilst the guidelines have been developed from experience with aircraft operations, the concepts are considered equally applicable to non-aircraft systems, such as those used on the surface or undersea environments. This document does not attempt to define or describe a comprehensive safety program for unmanned systems. System Safety is a system characteristic and a non-functional requirement. It has to be addressed at each level of system design, system integration and during each phase of system operation. System safety is achieved when the system operation does not cause inadvertent personnel injuries, destruction of the system or damage to the environment. Section 3 of the document contains an…
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Validation Methods for MIL-STD-1760 Mission Stores

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AS4270A
  • Current
Published 2017-06-27 by SAE International in United States
This document establishes techniques for validating that a mission store complies with the interface requirements delineated in MIL-STD-1760.
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Validation Methods for MIL-STD-1760 Aircraft Station Interfaces

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AS4764A
  • Current
Published 2017-06-27 by SAE International in United States
This document establishes techniques for validating that an aircraft station complies with the interface requirements delineated in MIL-STD-1760.
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Verification Methods for MIL-STD-1760E Aircraft Station Interfaces

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AS47643
  • Current
Published 2017-03-30 by SAE International in United States
This document establishes techniques for validating that an Aircraft Station Interface (ASI) complies with the interface requirements delineated in MIL-STD-1760 Revision E.
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Aircraft/Store Common Interface Control Document Format Standard

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AS5609A
  • Current
Published 2017-01-12 by SAE International in United States
This SAE Aerospace Standard (AS) defines the editorial format and policies necessary for the publication of Interface Control documents. The Common Interface Control Document Format Standard defines a common format for aircraft/store interface documents to foster increased interoperability. It is designed with the versatility to serve differing “ICD” philosophies and organizations. This aerospace standard defines the common technical data sections for the Common Interface Control Document Format down to the third header level for the majority of sub-sections. The Common Interface Control Document Format Aerospace Standard provides a structured document format in appendixes supported by example paragraphs, drawings, etc.
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Handbook: Standard Electrical and Logical Interface for Airborne Fuzing Systems

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AIR6234
  • Current
Published 2016-11-18 by SAE International in United States
This Handbook is intended to provide useful information on the application of AS5716A. It is for use by System Program Offices, aircraft prime contractors, avionics and store system designers, system integrators and equipment manufacturers and users. This Handbook was prepared to provide users of the standard of the rationale and principles considered during the development of the standard. It is anticipated that the handbook will serve to assist developers in introducing new technology to achieve compliance with the standard and the underlying principles of the standard. It is intended that the Handbook be used alongside the standard, as it does not contain significant extracts of the standard.
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Interface for Micro Munition (IMM) Handbook

AS-1B Aircraft Store Integration Committee
  • Aerospace Standard
  • AIR6114
  • Current
Published 2016-09-16 by SAE International in United States
This document was prepared by the SAE AS-1B1 IMM Task Group to explain and document background information and design decisions made during the development of AS5726. This handbook is published separately to preserve information that is not required or provided in the AS5726 but may be important to system designers to ensure interoperability between the Micro Munition Host and Micro Munition. As a handbook, it cannot be invoked as a requirement in a contract. The structure and numbering of this document mirrors that of AS5726 for the convenience of readers. Headings such as “Requirements” in this handbook should not be interpreted as invoking requirements.
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