NSN 6605-01-426-8522 · NIIN 014268522 · FSC 6605
NO DASHES 6605014268522
In Stock
INERTIAL NAVIGATION UNIT
Navigational Instruments
Application: C/KC-135 AIRCRAFT
Technical characteristics
14 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABFY | OVERALL DEPTH | INCHES NOMINAL 9.800 |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 7.000 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 7.000 |
| ACDC | CURRENT TYPE | DC |
| AGAV | END ITEM IDENTIFICATION | C/KC-135 AIRCRAFT |
| AXGY | MOUNTING METHOD | FIXED FLANGE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | NAVIGATION UNIT, INERTIAL-SATELITE SIGNALS |
| ELEC | VOLTAGE IN VOLTS | 28.0 |
| FEAT | SPECIAL FEATURES | 2/3A C-CELL GPS BATTERY INSTALLED;FRONT CONNECTOR PANEL:BUILT IN TEST; ELECTROSTATIC DISCHARGE SENSITIVE |
| FTLD | 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. |
| RDAL | REFERENCE DATA AND LITERATURE | DD FORM 61 |
| RTSE | RELATIONSHIP TO SIMILAR EQUIPMENT | 5 CHANNEL VS 12 CHANNEL P/N 34209200-40H4 |
| SUPP | SUPPLEMENTARY FEATURES | CONTAINS 3 RING LASER GYROS AND 3 ACCELEROMETERS IN A STRAP DOWN CONFIGURATION, EMBEDED GLOBAL POSITIONING SYSTEM RECIEVER |
| TMDN | TYPE/MODEL DESIGNATION | CN-1689(V)9/ASN |