| ELEC |
VOLTAGE IN VOLTS |
28.0 |
| ABKW |
OVERALL HEIGHT |
7.000 INCHES NOMINAL |
| FEAT |
SPECIAL FEATURES |
2/3A C-CELL GPS BATTERY INSTALLED;FRONT CONNECTOR PANEL:BUILT IN TEST; ELECTROSTATIC DISCHARGE SENSITIVE |
| TMDN |
TYPE/MODEL DESIGNATION |
CN-1689(V)9/ASN |
| ACDC |
CURRENT TYPE |
DC |
| RDAL |
REFERENCE DATA AND LITERATURE |
DD FORM 61 |
| RTSE |
RELATIONSHIP TO SIMILAR EQUIPMENT |
5 CHANNEL VS 12 CHANNEL P/N 34209200-40H4 |
| CXCY |
PART NAME ASSIGNED BY CONTROLLING AGENCY |
NAVIGATION UNIT, INERTIAL-SATELITE SIGNALS |
| ABFY |
OVERALL DEPTH |
9.800 INCHES NOMINAL |
| AGAV |
END ITEM IDENTIFICATION |
C/KC-135 AIRCRAFT |
| ABMK |
OVERALL WIDTH |
7.000 INCHES NOMINAL |
| SUPP |
SUPPLEMENTARY FEATURES |
CONTAINS 3 RING LASER GYROS AND 3 ACCELEROMETERS IN A STRAP DOWN CONFIGURATION, EMBEDED GLOBAL POSITIONING SYSTEM RECIEVER |
| 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. |
| AXGY |
MOUNTING METHOD |
FIXED FLANGE |