We are pleased to offer procurement for Honeywell International Inc part number CN-1689-V-9-ASN here on NSN Portal, a Inertial Navigation product that is listed with the NSN 6605-01-426-8522 for ease of identification. You have reached our Request for Quote (RFQ) form for this listing, where you are encouraged to submit details on your requirements to receive tailored purchasing options from our staff. As you will see, we ask that you offer key information on your pricing target, desired quantity, and more, as this will ensure that the representative who responds to your request is able to provide the most fitting solutions for your needs.
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Whether you procure part number CN-1689-V-9-ASN or other NSN products from our website, you can rest assured that we uphold full traceability for all items. For example, this particular listing traces back to Honeywell International Inc through the CAGE Code 0BFA5, as well as falls under FSC 6605 Navigational Instruments based on having the NSN 6605-01-426-8522. Furthermore, every purchase will be delivered with any applicable qualifying certifications or manufacturer trace documentation as per our NO CHINA SOURCING pledge. If you are ready to experience why professionals rely on us for their needs, request a quote for part number CN-1689-V-9-ASN today and take advantage of our industry-leading services.
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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