To receive competitive purchasing options on part number CN-1689-V-9-ASN by Joint Electronics Type Designation System, look no further than NSN Direct. For your reference, this item has the NSN 6605-01-426-8522 and is listed with the description “Inertial Navigation.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other Joint Electronics Type Designation System parts produced under the CAGE Code 80058, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number CN-1689-V-9-ASN, you can glean from the first four digits of its NSN 6605-01-426-8522 that it belongs to the FSC 6605 Navigational Instruments. This being said, do not hesitate to request quotes on part number CN-1689-V-9-ASN and any other NSN parts that we feature to experience unrivaled procurement.
| MRC | Criteria | Characteristic |
|---|---|---|
| ABFY | OVERALL DEPTH | 9.800 INCHES NOMINAL |
| SUPP | III SUPPLEMENTARY FEATURES | CONTAINS 3 RING LASER GYROS AND 3 ACCELEROMETERS IN A STRAP DOWN CONFIGURATION, EMBEDED GLOBAL POSITIONING SYSTEM RECIEVER |
| ABMK | OVERALL WIDTH | 7.000 INCHES NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | C/KC-135 AIRCRAFT |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | NAVIGATION UNIT, INERTIAL-SATELITE SIGNALS |
| TMDN | III TYPE/MODEL DESIGNATION | CN-1689(V)9/ASN |
| ACDC | CURRENT TYPE | DC |
| FTLD | III FUNCTIONAL DESCRIPTION | EMBEDDED GPS/INS (EGI) UNIT IS A SELF-CONTAINED ALL-ATTITUDE NAVIGATION LINE REPLACEABLE UNIT PROVIDING OUTPUTS OF ACCELERATION, ATTITUDE (AZIMUTH, PITCH, ROLL), ATTITUDE RATES, HEADING, POSITION, VELOCITY, ASSOCIATED TIME TAG INFORMATION, AND UNIVERSAL TIME COORDINATED (UTC) SYNCHRONIZED TIME VIA EXTERNALLY CONTROLLED MIL-STD-1553B DUAL MULTIPLEX DATA BUS WHICH REQUESTS DATA & TRANSMITS UPDATED DATA BASED UPON THE REQUIREMENTS OF THE INTERFACING AVIONICS SYSETEMS. EGI PROVIDES SIMULTANEOUS INS ONLY, BLENDED GPS/INS & GPS ONLY POSITION SOLUTIONS. |
| ELEC | VOLTAGE IN VOLTS | 28.0 |
| AXGY | MOUNTING METHOD | FIXED FLANGE |
| RTSE | III RELATIONSHIP TO SIMILAR EQUIPMENT | 5 CHANNEL VS 12 CHANNEL P/N 34209200-40H4 |
| ABKW | OVERALL HEIGHT | 7.000 INCHES NOMINAL |
| RDAL | III REFERENCE DATA AND LITERATURE | DD FORM 61 |
| FEAT | SPECIAL FEATURES | 2/3A C-CELL GPS BATTERY INSTALLED;FRONT CONNECTOR PANEL:BUILT IN TEST; ELECTROSTATIC DISCHARGE SENSITIVE |
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