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- NSN 6605-01-461-6592
6605-01-461-6592
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.)
6605-01-461-6592 Properties
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NSN:6605-01-461-6592
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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:--
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Overall Length:15.187 inches
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Overall Height:7.625 inches
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Overall Width:6.750 inches
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Current Type:Dc
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End Application:F117 aircraft
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Voltage In Volts:115.0 and 200.0
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Special Features:Receives 26v, 400hz single phase synchro reference power; aircraft 28v DC discrete power excluding battery back up power
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Frequency In Hertz:400.0
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Functional Description:4capable of determining position, velocity, heading, accelerations, body rates, and attitude in the autonomous mode from take off to landing after a ground alignment in the following modes: gyrocompass, stored heading, best available true heading
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Supplementary Features:Electrostatic discharge sensitive