Thank you for your vested interest in part number 34200600-30H4, one of the many Inertial Navigation items we offer from Joint Electronics Type Designation System. On this page, you can easily fill out a Request for Quote (RFQ) form for NSN 6605014268522 that caters to your requirements. Simply fill out the form below with details about your situation, such as desired part quantity and expected shipping deadline, and a dedicated account manager will reach out to you with a competitive quote for your comparisons in 15 minutes or less. For more information, you are also welcome to contact us at any time via phone or email, as we are available around the clock!
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Aside from the NSN 6605-01-426-8522, we carry a host of other parts within the Federal Supply Class 6605 Navigational Instruments. Each of these items are fully traceable and have been sourced from credible manufacturers whom we trust, including Joint Electronics Type Designation System with the CAGE Code 80058. Additionally, you can count on us for quality-evaluated products that come delivered with their qualifying certifications and manufacturer trace documentation, as applicable. Regardless of your situation, NSN Matrix is here to assist you with all the logistics behind part procurement, so kick off the purchasing process with us today to learn how we can get you the parts your operations require ASAP!
| 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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