At Orbit NSN, we offer an expansive inventory of Inertial Navigation components by Joint Electronics Type Designation System, including part number 34200600-30H4-SM, and many others. On this page, you can complete and submit a quote request form for this part number and others with the NSN 6605014268522 to receive a customized solution within 15 minutes or less of submission. All we ask is that you include relevant information while filling out this form, such as your desired part quantity and budget parameters, so our dedicated staff can best respond with a quote that suits your needs and restrictions alike.
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Quality is the cornerstone of our operations at Orbit NSN, and as such, we proudly operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation, in addition to adhering to a strict NO CHINA SOURCING policy. To make your search simple, our catalogs feature items with CAGE Code 80058 and FSC 6605 Navigational Instruments so that you always know you are procuring the exact items you need. To learn more about components with the NSN 6605-01-426-8522, such as this part manufactured by Joint Electronics Type Designation System, give us a call or email at any time, and a dedicated team member will be more than happy to assist you however they can through the procurement process. Get started today to see why our customers continue to rely on our top-notch products and services for all their operational needs.
| 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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