MIL-STD-1760 Aircraft/Store Electrical Interconnection System defines a standardized electrical interface between a military aircraft and its carriage stores. Carriage stores range from weapons, such as GBU-31 JDAM, to pods, such as AN/AAQ-14 LANTIRN, to drop tanks . Prior to adoption and widespread use of MIL-STD-1760, new store types were added to aircraft using dissimilar, proprietary interfaces. This greatly complicated the aircraft equipment used to control and monitor the store while it was attached to the aircraft: the stores management system, or SMS.
23-505: MIL-STD-1760 defines the electrical characteristics of the signals at the interface, as well as the connector and pin assignments of all of the signals used in the interface. The connectors are designed for quick and reliable release of the store from the aircraft. Weapon stores are typically released only when the aircraft is attacking a target, under command of signals generated by the SMS. All types of stores may be released during jettison, which
46-462: A PCB . The technician probes each pin of the component in turn, comparing the expected signal on each pin to the actual signal on that pin. Viewed from the front (outside) of Female Type A USB receptacle: Warhead A warhead is the section of a device that contains the explosive agent or toxic (biological, chemical, or nuclear) material that is delivered by a missile , rocket , torpedo , or bomb . Types of warheads include: Often,
69-465: A rate of one megabaud . The MIL-STD-1553 interface includes four signal lines, five lines used to assign one of 31 communications addresses to the store (one address is reserved), and address parity and return lines, for a total of 11 lines. To support weapons applications such as digitized video, and transfers of terrain maps, target images, and program files, Revision E of MIL-STD-1760 includes an option for higher speed data communication. This option,
92-500: Is a non-offensive release that can be used, for example, to lighten the weight of the aircraft during an emergency. There are five main groups of MIL-STD-1760 signals: Note that the standard describes three groups: A) the signal lines (consisting of the high & low bandwidth, MIL-STD-1553 communications, and fiber optic signals); B) the discrete lines (consisting of the MIL-STD-1553 discretes and other discrete signals); and C)
115-400: Is used as follows with a notional weapon that uses GPS for terminal guidance. Prior to activating any of the store's interface signals, the aircraft will examine the interlock discretes to ensure that the store is attached to the aircraft, thereby preventing the ground crew from being subjected to an electrical shock hazard while servicing the aircraft. The interface will be energized to supply
138-526: Is used by the aircraft to determine whether the store is attached to the aircraft. This interface uses two signals, the Interlock, and the Interlock Return. These signals are simply connected together within the store, and when the store is released from the aircraft this connection is broken on the aircraft side. The aircraft determines the presence of the store by measuring the continuity between
161-567: The High Speed Network for MIL-STD-1760 (High-Speed 1760), is defined by SAE standard AS5653. High-Speed 1760 specifies a gigabit-speed interface based on Fibre Channel , operating at 1.0625 Gbit/s over a pair of 75 ohm coax cables. The Fibre Channel upper layer protocols for High-Speed 1760 are FC-AE-1553, based on MIL-STD-1553, for command and control messages and file transfers; and FC-AV for video and audio. The high and low bandwidth signals are for routing analog signals between
184-549: The MIL-STD-1553 interface to send current position and time to the weapon, and a high bandwidth signal to route the GPS satellite signal from a topside aircraft antenna to the weapon. Just prior to release, the aircraft activates the Release Consent discrete and sends the weapon an arming command using the MIL-STD-1553 interface. The SMS will verify that the weapon release conditions have all been fulfilled, and it will activate
207-490: The aircraft after the bomb hooks open). The MIL-STD-1760 connector will release as the bomb falls away from the aircraft, and the SMS will detect that the bomb has separated by the open circuit between the Interlock and Interlock Return discrete signals. Pinout In electronics , a pinout (sometimes written " pin-out ") is a cross-reference between the contacts, or pins , of an electrical connector or electronic component , and their functions. "Pinout" now supersedes
230-498: The aircraft and the store. Note that either the aircraft or the store can be the source of the signal. The high bandwidth signals are intended for carrying video and other high frequency signals, such as those transmitted by the Global Positioning System (GPS). The low bandwidth signals are intended for carrying audio and other low frequency signals. There are two sets of discrete signals. The Interlock discrete
253-454: The aircraft can determine whether the store's auxiliary power connector is attached to the aircraft. MIL-STD-1553 is a military standard for the Digital time division command/response multiplex data bus that has been used since the 1970s for data communications between avionics devices on American military aircraft. It is a dual-redundant differential serial interface that operates at
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#1732772617650276-530: The connector (where wires are attached) or the "mating face" of the connector. Published pinouts, which are particularly important when different manufacturers want to interconnect their products using open standards , are typically provided by the connector or equipment manufacturer. However, some pinouts are provided by 3rd parties since the manufacturer does not well document some connectors. While repairing electronic devices, an electronics technician uses electronic test equipment to " pin out " each component on
299-476: The contact on the other connector with the same function. If contacts of disparate functions are allowed to make contact, the connection may fail, and damage may result. Therefore, pinouts are a vital reference when building and testing connectors, cables, and adapters. Suppose one has specified wires within a cable (for instance, the colored Ethernet cable wires in ANSI/TIA-568 T568A ). In that case,
322-568: The last two supplies, however, if both are made available, then they are never made active simultaneously. The MIL-STD-1760 interface provides power through the primary interface (two off 28 VDC and either one or both 115/200V VAC and 270 VDC), where it is routed to the store along with all of the other signal types. The standard also allows for an optional auxiliary power interface (1 off 28 VDC and either 115/200 VAC or 270 VDC) for stores with more demanding power requirements. The auxiliary power interface includes its own interlock discrete signals so that
345-452: The order in which different color wires are attached to pins of an electrical connector defines the wiring scheme. In any multi-pin connector, there are multiple ways to map wires to pins, so different configurations may be created that superficially look identical but function differently. Pinouts define these configurations. Many connectors have multiple standard pinouts in use for different manufacturers or applications. While one usage of
368-470: The power lines (which are the same as those described here). In common practice, an aircraft will support most of the MIL-STD-1760 signals, whereas the store needs to accommodate only those signals it needs to perform its mission. As a result, stores typically use only a subset of the MIL-STD-1760 signals. MIL-STD-1760 was intended to support both current needs as well as to provide growth capability as
391-420: The signals (not part of the MIL-STD-1760 interface) that cause the weapon to be released. In the case of a bomb, this is typically done by energizing an electro-explosive device that simultaneously opens the hooks that hold the bomb on the aircraft during carriage, and also operate a plunger that pushes the bomb away from the aircraft (at high speeds there is a tendency for the weapon to remain in close proximity to
414-414: The technology matures. MIL-STD-1760 defines a Class I aircraft interface, which has four high bandwidth and two fiber optic interfaces, and a Class II interface, which has only two high bandwidth and no fiber optic interfaces. The MIL-STD-704 power connections provide the store with access to 28 VDC , three-phase wye 400 Hz 115/200 VAC , and 270 VDC aircraft power; it is usual to route only one of
437-715: The term "basing diagram" which was the standard terminology used by the manufacturers of vacuum tubes and the RMA. The RMA started its standardization in 1934, collecting and correlating tube data for registration at what was to become the EIA . The EIA (Electronic Industries Alliance) now has many sectors reporting to it and sets what is known as EIA standards where all registered pinouts and registered jacks can be found. The functions of contacts in electrical connectors, be they power- or signaling-related, must be specified for connectors to be interchangeable. Each connector contact must mate with
460-522: The two signals. Certain stores, typically weapons, may be commanded into modes that can be hazardous if not managed properly, such as the arming of a warhead . Activation of the Release Consent discrete signal is used to ensure that the store will only accept such a command when it is authorized to do so. The fiber optic interface is intended for much higher digital communications speeds than can be supported by MIL-STD-1553, such as Fibre Channel, which can operate at gigabaud rates. The MIL-STD-1760 interface
483-403: The weapon to report its status, and will continue with commands that ready the weapon for its mission, such as navigation initialization and target coordinates. The weapon's GPS receiver will be able to lock onto the signals from GPS satellites and resolve its position much more quickly after it separates from the aircraft if it is initialized with the current position and time. The aircraft may use
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#1732772617650506-448: The weapon with electrical power when the air crew determines that hostilities are imminent. The weapon electronics will initialize itself, including running a battery of self tests and starting its MIL-STD-1553 communications interface. The weapon will read its address from the settings on its MIL-STD-1760 interface and will start to listen for MIL-STD-1553 commands to that address from the SMS. These commands will commence with requests for
529-408: The word pin is to refer to electrical contacts of, specifically, the male gender , its usage in pinout does not imply gender: the contact-to-function cross-reference for a connector that has only female socket contacts is still called a pinout . The pinout can typically be shown as a table or diagram. However, it is necessary to clarify how to view the diagram, stating if it shows the backside of
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