CN-1689-V-9-ASN by Joint Electronics Type Designation System with NSN 6605-01-426-8522 - Submit a Quote

Part Number:  CN-1689-V-9-ASN
Alternate P/N:  CN1689V9ASN
Item Name :  inertial navigation
CAGE Code:  80058
INC Code:  53294

ASAP Aviation Procurement is pleased to announce that part number CN-1689-V-9-ASN of NSN 6605-01-426-8522 is now available and in stock. We can get you one of the fastest and most competitive quotes on this part. Part number CN-1689-V-9-ASN is a Inertial Navigation manufactured by Joint Electronics Type Designation System under CAGE Code 80058. Simply fill out the Request for Quote (RFQ) form provided here to get started on your quote. In order to make sure that we get you your quote in a timely manner, please take the time to make sure that all fields are completely filled out, particularly the asterisk-marked (*) fields like Parts Needed By and Quantity (ea). 

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Disclaimer: This is a quotation for the goods listed above. This quotation is meant as an estimate and does not reflect a final bill or invoice. All quotations are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor. This quotation is subject to the ASAP Semiconductor Terms & Conditions available at https://www.asapsemi.com/customer-terms-and-conditions/. All United States Government and Department of Defense bids are quoted as CAGE code 6RE77 from ASAP Semiconductor’s Anaheim, California facility. Any quotation from ASAP Semiconductor without 6RE77 is void.

Characteristics Data of NSN 6605-01-426-8522, 6605014268522

MRCCriteriaCharacteristic
ABFYOVERALL DEPTH9.800 INCHES NOMINAL
SUPPIII SUPPLEMENTARY FEATURESCONTAINS 3 RING LASER GYROS AND 3 ACCELEROMETERS IN A STRAP DOWN CONFIGURATION, EMBEDED GLOBAL POSITIONING SYSTEM RECIEVER
ABMKOVERALL WIDTH7.000 INCHES NOMINAL
AGAVIII END ITEM IDENTIFICATIONC/KC-135 AIRCRAFT
CXCYIII PART NAME ASSIGNED BY CONTROLLING AGENCYNAVIGATION UNIT, INERTIAL-SATELITE SIGNALS
TMDNIII TYPE/MODEL DESIGNATIONCN-1689(V)9/ASN
ACDCCURRENT TYPEDC
FTLDIII FUNCTIONAL DESCRIPTIONEMBEDDED 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.
ELECVOLTAGE IN VOLTS28.0
AXGYMOUNTING METHODFIXED FLANGE
RTSEIII RELATIONSHIP TO SIMILAR EQUIPMENT5 CHANNEL VS 12 CHANNEL P/N 34209200-40H4
ABKWOVERALL HEIGHT7.000 INCHES NOMINAL
RDALIII REFERENCE DATA AND LITERATUREDD FORM 61
FEATSPECIAL FEATURES2/3A C-CELL GPS BATTERY INSTALLED;FRONT CONNECTOR PANEL:BUILT IN TEST; ELECTROSTATIC DISCHARGE SENSITIVE

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