Thank you for your interest in part number 34200600-30H4, a component manufactured by Joint Electronics Type Designation System that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 6605-01-426-8522 and features the description “Inertial Navigation.” To request a quote for part number 34200600-30H4, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 6605-01-426-8522 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from Joint Electronics Type Designation System, which is associated with the CAGECode 80058. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 6605 Navigational Instruments part number 34200600-30H4.
| 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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