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th a subaddress field of 19 and 27 (decimal) shall be reserved for control of U.S. nuclear weapons. For all aircraft with a requirement to control U.S. nuclear weapons, usage shall conform to specifications accompanying the U.S nuclear weapon carriage requirement. For all other applications of MIL-STD-1760, the requirement is that these subaddresses shall not be used. C.4.2.2.5. Nuclear weapon monitor Transmit messages with a subaddress field of 19 and 27 (decimal) shall be reserved for monitor of U.S. nuclear weapons. For all aircraft with a requirement to control U.S. nuclear weapons, usage shall conform to specifications accompanying the U.S nuclear weapon carriage requirement. For all other applications of MIL-STD-1760, the requirement is that these Source: https://assist.dla.mil -- Do
MIL-STD-1760, the requirement is that these Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:48Z Check the source to verify that this is the current version before use. MIL-STD-1760F APPENDIX C MIL-STD-1553 DATA BUS COMMUNICATION RULES AND MESSAGE REQUIREMENTS 146 subaddresses shall not be used. C.4.2.2.6. Aircraft description See B.4.2.2.4. The aircraft description message shall use subaddress 1 (decimal) and comply with the format of TABLE B-XXIX. C.4.2.3. Mass data transfer messages Aircraft and stores which require Mass Data Transfer (MDT) operations shall use the applicable operations defined herein. MDT shall be implemented through the use of three data message types. The Transfer Control (TC) message (C.4.2.3.2.1) is a standard receive message for controlling the transfer
agreements. When changes to, revision, or cancellation of this standard are proposed, the preparing activity must coordinate the action with the U.S. National Point of Contact for the international standardization agreement, as identified in the ASSIST database at http://assist.dla.mil. Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:48Z Check the source to verify that this is the current version before use. MIL-STD-1760F 69 a. STANAG 3350, Analogue Video Standard for Aircraft System Applications b. STANAG 3837, Aircraft Stores Electrical Interconnection System c. STANAG 3838, Digital Time Division Command/Response Multiplex Data Bus. 6.4 Tailoring Guidance MIL-STD-1760 defines a standard connector and signal interface between stores and aircraft. As such, most of the requirem
n of the arming unit should correspond to the geometry outlined in MIL-A-8591 and MIL-STD-2088, either attached to pylon or aircraft structure. Access should be provided vertically to permit the elec- tric fuze arming cable connection to be madeby hand after the weapon is mounted on therack. 5.2.9.3 Diuital arming. For new store applications using MIL-STD-1760 and its associated MIL-STD-1553 multiplexed digital data inter- face, the transfer of arming commands from aircraft to the store should occur. through the MIL-STD-1760 interface. The transfer.of digitally encoded arming commands can be protected to a high level by the error detection coding methods described in MIL-STD-1760 and through the use of Preset, Verify, . Execute (PVE) command and monitor sequences. The use of digital arming
rget motion, − Four target, closed loop radar target simulator with dynamic radar cross section, jet engine modulation, electronic countermeasures, and clutter signatures, − 6174 open loop, multiplexed threat radar emitters, − MIL-STD-1760 weapons and aircraft simulators, − Two, 10-channel, differential Global Positioning System constellations and jammers, and − Test instrumentation systems, include MIL-STD-1760, MIL-STD-1553, H009, AIM- 7/9/120 umbilical and telemetry analyses. D.4.2 Air Force Research Laboratories (AFRL) D.4.2.1 Information Directorate The Newport Research Facility is used to evaluate antennas and antenna systems in a far-field "free space" environment, to determine radiation pattern changes due to airframe effects, for the measurement of antenna-to-antenna isolation, an
) MIL-STD-1512 Electroexplosive Subsystems, Electrically Initiated, Design Requirements and Test Methods MIL-STD-1670 Environmental Criteria and Guidelines for Air-Launched Weapons MIL-STD-1760 Interface Standard for Aircraft/Store Electrical Interconnection System MIL-STD-1795 Lightning Protection of Aerospace Vehicles and Hardware MIL-STD-1818 Electromagnetic Effects Requirements for Systems MIL-STD-2105 Hazard Assessment Tests for Non-Nuclear Munitions MIL-STD-2167 Defense System Software Development (Canceled) MIL-STD-38784 Standard Practice for Manuals, Technical: General Style and Format Requirements HANDBOOKS MIL-HDBK-235-1 Electromagnetic (Radiated) Environment Considerations for Design and Procurement of Electrical and Electronic Equipment, Subsystems and Systems MIL-HDBK-244 Guid
://assist.dla.mil -- Downloaded: 2026-07-20T01:47Z Check the source to verify that this is the current version before use. MIL-HDBK-516D 10 MIL-STD-1587 Material and Process Requirements for Aerospace Weapons Systems MIL-STD-1760 Aircraft/Store Electrical Interconnection System MIL-STD-1787 Aircraft Display Symbology MIL-STD-1791 Designing for Internal Aerial Delivery in Fixed Wing Aircraft MIL-STD-1791-1 Criteria for Nonstandard Airdrop Equipment and Payloads MIL-STD-1796 Avionics Integrity Program (AVIP) MIL-STD-1797 Flying Qualities of Piloted Aircraft MIL-STD-1798 Mechanical Equipment and Subsystems Integrity Program MIL-STD-3009 Lighting, Aircraft, Night Vision Imaging System (NVIS) Compatible MIL-STD-3013 Glossary of Definitions, Ground Rules, and Mission Profiles to Define Air Vehic
safe. (T-2) Battle damage checks are not required at night or in IMC. 5.4.12.2. If unable to confirm ordnance expenditure on the range, perform a visual bomb check. The aircrew, RCO, JTAC, B-1 Stores Management System, B-2 Mission Management System, B-52 Stores Management Overlay for MIL-STD-1760 weapons, or another flight member can all confirm ordnance expenditure. If visual confirmation is not feasible (for example, night), follow hung ordnance or unconfirmed hung ordnance procedures. (T-2) 5.4.13. Recovery From Delivery. Execute recoveries from weapons deliveries according to safe escape maneuvers described in the applicable TO series 1-34-1-1 aircraft-specific TOs. Recoveries will observe minimum altitudes consistent with safe escape, fuse arming, and the weapon delivery minimum alti
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