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MIL-HDBK-244A 6 apr 90.pdf

MIL-HDBK-244A 6 apr 90.pdf

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<strong>MIL</strong>-<strong>HDBK</strong>-<strong>244A</strong><br />

(1) Store sensing and identification- Depending on<br />

system requirements and aircraft geometry, considerations should be given to<br />

store sensing devices to provide positive indicationof store present condition<br />

on the suspension equipment, particularly in the case of a bomb bay,<br />

fuselage or wing centerline station that cannot be observed by the.crew inflight.<br />

This information is necessary to the pilot to indicate the completion<br />

of an attack and to confirm aircraft loading and weapon status. <strong>MIL</strong>-STD-1760<br />

provides mechanism for automaticallydetermining the identificationof a<br />

store connected to’the aircraft. <strong>MIL</strong>-STD-1760 also includes a mechanism<br />

(interlock interface) for verifying that the store is electrically mated to<br />

the aircraft. (This interlock interface, by itself, does not provide a reliable<br />

indication that the store has physically separated from the aircraft<br />

or is not physically present at the station.)<br />

_<br />

5.1.5.1 Safety devices. The weapon should be designed to incorporate<br />

safety devices that will preclude premature (inadvertent) launch or<br />

premature detonation, and ensure positive lock of the attachment of the suspension<br />

equipment to the aircraft structure, and the engagement of the stores<br />

to the suspension equipment. These safety devices may be broadly classified<br />

as inflight and ground type.<br />

. .,.<br />

5.1.5.1.1 In-flight. The weapon should be designed to incorporate<br />

safety devices to preclude premature (inadvertent) launch or premature detonation.<br />

The aircraft side of the interface should provide appropriate controls<br />

to ensure proper and positive actuation of any safety devices controllable<br />

by the aircrew. The system should be designed to ensure that safe<br />

separation is accomplished prior to weapon in-flight arming or fuzing.<br />

.<br />

-<br />

5.1.5.1.1.1 Interlocks. Mechanical or electrical interlocks should be<br />

applied to prevent inadvertent selection and attempted launchljettisonof<br />

stores. Interlocks that can prevent store release or jettison should also be<br />

incorporated into suspension equipment, bomb bay doors or any movable surface<br />

of the aircraft (such as extended landing gear).<br />

5.1.5.1.1.2 Jettison. The interface should be so designed that positive<br />

and emergencyjettison of.all stores can be accomplished in an unarmed condition<br />

by the pilot in event of flight emergencies. The stores must be controllable<br />

for jettison or launch in an unarmed condition where separationmay<br />

be necessary in friendly territory.<br />

5.1.5.1.2 Ground. Mechanical devices should be applied at the aircraft/weapon<br />

interface to ensure positive lock of the attachment of the suspension<br />

equipment to the aircraft structure, and the engagement of the stores<br />

33<br />

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