MIL-STD-1822A(USAF)
6.5 Nuclear Compatibility Certification Reports.
6.5.1 Aircraft Monitor and Control (AMAC) Design Approval Report (DAR).
This report defines and analyzes the aircraft system which controls the interface between the aircraft and the nuclear weapon. It should be submitted in two parts as described below. DI- NUOR-81408, Aircraft Monitor and Control (AMAC) Preliminary Design Report (PDR) and Final Design Approval Report (FDAR), applies to these requirements. Deliverable data identified on the DD Form 1423 should be prepared in accordance with instructions specified in this DID and prepared to include the following:
6.5.1.1 Preliminary Design Approval Report.
This report should describe in as much detail as possible the design details of the proposed AMAC system, which consists of the electrical controls and avionics required to monitor, safe, or pre-arm a nuclear weapon prior to release. It should be submitted as soon as the design baseline of the AMAC system has been established. Normally, this should be in conjunction with the weapon system preliminary design review.
6.5.1.2 Final Design Approval Report.
This report should include a complete design analysis detailing all the circuits and components employed, and an analysis showing compliance with the applicable nuclear weapons requirements. All electrical analyses should be based on worst expected conditions of aircraft direct current loads, power input conditions, and temperature conditions. The complete power distribution analysis should be performed using only the main alternating current generator(s). All constraints used in the analyses should be substantiated in the report by cross-referencing applicable test reports, specification sheets, and military standard drawings. The design should represent the production design to be deployed, and no changes can be made to the nuclear interface defined in this report unless a revised AMAC report first provides a second review and is approved in writing by the authorized agencies (Single Manager and the AFNWC's Certification Manager). In order to support the ACCD release, the FDAR should be completed and submitted to the Single Manager at least 270 days prior to the nuclear certification need date.
6.5.2 Aircraft Electrical Interface Control Drawing (EICD).
The EICD should define the physical, electrical power, and logical signal interfaces between the avionics components at the DoE/Air Force interfaces. They should cover all types of electrical interfaces in the monitor and control circuits of nuclear weapons, whether discrete lines or multiplex data buses. DI-NUOR-81410, Aircraft EICD, applies to these requirements. Deliverable data identified on the DD Form 1423 should be prepared in accordance with the instructions specified in this DID.
6.5.3 Aircraft Mechanical Interface Control Drawing (MICD).
The MICD should define the physical and mechanical interfaces between the aircraft and nuclear weapons. They should cover dimensions, clearances, forces, installations, etc., associated with the weapons and suspension and release equipment. DI-NUOR-81407, Aircraft MICD, applies to these requirements. Deliverable data identified on the DD Form 1423 should be prepared in accordance with the instructions specified in this DID.
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