Thank you for taking an interest in the military and defense parts, aerospace parts, and other NSN part offerings we offer here on ASAP Rotable Parts. You have reached the request for quote (RFQ) page for Joint Electronics Type Designation System part number 34200600-30H4, a Inertial Navigation item that is listed alongside the NSN 6605014268522 for an ease of identification. If you would like to receive more information on this part alongside purchasing options, please fill out and submit the form provided on this page at your earliest convenience. When you provide us with details like your target price, expected shipping time frame, and more, we can best formulate and present a quote on part number 34200600-30H4 that caters to you.
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To ensure an ease of part identification and procurement, we list all offerings with as much information as we can. For example, part number 34200600-30H4 is specifically produced under CAGE Code 80058, that of which identifies the specific facility where this traces back to. Additionally, with the first digits of NSN 6605-01-426-8522, one can determine that this item belongs to FSC 6605 Navigational Instruments. With such information, you can always rest assured that you are procuring exactly what you require. As such, get started on the quotation process today, and see why so many customers steadily choose us for fulfillment.
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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