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- NSN 6605-01-511-3424
6605-01-511-3424
Description: Inertial Navigation Unit
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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.)
6605-01-511-3424 Properties
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NSN:6605-01-511-3424
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Description:Inertial Navigation Unit
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Shelf Life:N/A
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DEMIL:DEMIL/MLI
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UOM:EA
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Overall Depth:11.000 inches
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Overall Length:7.000 inches
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Overall Height:7.000 inches
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Current Type:Dc
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End Application:F-15 aircraft
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Mounting Method:Bolt clamp
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Part Name Assigned By Controlling Agency:Navigation unit, inertial-satellite signals
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Voltage In Volts:28.0
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Special Features:Contains 3 ring laser gyros; 3 accelerometers in a strap down configuration, embedded global postion reciever, 1553/b mutiplex bus, built in test, f-15 avionics interface card
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Functional Description:F15 saasm embedded gps/ins (egi) unit is a self contained all-attitude line replaceable navigation unit. Povides the following outputs: acceleration, attitude (azimuth, pitch, roll), attitude rates and universal time coordinated. Provides inertial, blended & gps only position solutions
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Reference Data And Literature:Ddform61
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Type/model Designation:Cn-168 (v) 15/asn
