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- NSN 6605-01-339-9252
6605-01-339-9252
Description: Navigati Inertial Reference 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.)
6605-01-339-9252 Properties
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NSN:6605-01-339-9252
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Description:Navigati Inertial Reference 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:18.100 inches
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Overall Height:9.120 inches
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Overall Width:8.000 inches
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Current Type:Dc
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End Application:C-17 aircraft
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Special Features:Strapdown system; utilizes ring laser gyros; dual digital interface (2 remote terminals); one interfaces with mission bus; one interfaces with efcs bus; built-in battery charger; 28 vdc from aircraft power; 28 vdc from battery; rack mounted; electrostatic discharge sensative
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Functional Description:The inertial reference unit utilizes a set of accelerometers and ring laser gyros to sense aircraft rates and accelerations, computes and provides aircraft attitude, attitude rates, true heading, velocity, acceleration and position information to the c-17 mission computer for navigation and display purposes; attitude rates, heading, ground speed, flight path angle, inertial angle of attack (aoa), aoa rate, side slip angle and side slip angle rate