MIL-HDBK-244A 6 apr 90.pdf
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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