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- NSN 5895-01-652-4881
5895-01-652-4881
Description: Guidance Control Group
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Export Restrictions
Any part(s) quoted or sold by MilSpec.parts and re-sold (to a third party) CANNOT be sold to a USA embargoed country, company, entity, or person(s). Depending on the ECCN, these commodities may require export license or exception. Diversion contrary to U.S. law is prohibited. Unless otherwise noted, this sale, order or quote may include Munitions List Items (MLI) or Commerce Controlled List Items (CCLI). MLI/CCLI property is controlled by the US Government and in many cases cannot be transferred (exported, sold or given) to a foreign country, a non-US Citizen/National or a non- Permanent US Resident without a valid State/Commerce Department export authorization. It is the responsibility of (the Purchaser) to determine what the applicable requirements may be, to obtain all necessary authorizations, licenses or approvals and are subject to both review and acceptance by MilSpec.parts. The use, disposition, export and re-export of the property covered or included in this sale, order or quote is subject to the provisions of law referenced in End-Use Certificate DLA form 1822, DEC 2001, including, but not limited to, the Arms Export Control Act (22 USC 2751 et seq.); Export Administration Act of 1979 (50 USC App. 2401 et seq.) as contained under Executive Order 12924; International Traffic in Arms Regulations (22 CFR 120 et seq.); Export Administration Regulations (15 CFR 730 et seq.); Foreign Assets Control Regulations (31 CFR 500 et seq.) and the Espionage Act (18 USC 793 et seq.)
5895-01-652-4881 Properties
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NSN:5895-01-652-4881
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Description:Guidance Control Group
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Shelf Life:N/A
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DEMIL:DEMIL/MLI
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UOM:--
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Component Quantity:2
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Container Type:Case
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Part Name Assigned By Controlling Agency:Autonomous guidance unit (agu)
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Special Features:Has fourcorner riser brackets that transfer load from the 2k parachute to the 2k firefly payload suspension sling; the power source on board is a pair of 12 volt sealed lead acid (sla) batteries connected in series to provide 24 volts; each battery has a capacity of 35 watts and 8.5 sh; a operational draw of 160 amps is possible when both motors controllers are active; has been tested under dynamic loading scenarios to withstand up to 10gs (25000 lb) during opeing shock under the mamimum suspended payload; is a programmable steering unit that contains a gps receiver; a magnetic compass; an inertial measurement unit (imu) and motor-driven control line spools to steer the 2 k firefly system to the intended impact point; powered by a non-replaceable, rechargeable dry cell battery; the agu activation cable is pulled from the activation block upon parachute deployment and initiaes power to the agu