NSN 6605-01-511-3424 · NIIN 015113424 · FSC 6605
NO DASHES 6605015113424
In Stock
INERTIAL NAVIGATION UNIT
Navigational Instruments
Application: F-15 AIRCRAFT
Technical characteristics
12 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 11.000 |
| ABHP | OVERALL LENGTH | INCHES NOMINAL 7.000 |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 7.000 |
| ACDC | CURRENT TYPE | DC |
| AGAV | END ITEM IDENTIFICATION | F-15 AIRCRAFT |
| AXGY | MOUNTING METHOD | BOLT CLAMP |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | NAVIGATION UNIT,INERTIAL-SATELLITE SIGNALS |
| ELEC | VOLTAGE IN VOLTS | 28.0 |
| FEAT | SPECIAL FEATURES | CONTAINS 3 RING LASER GYROS; 3 ACCELEROMETERS IN A STRAP DOWN CONFIGURATION, EMBEDDED GLOBAL POSTION RECIEVER, 1553/B MUTIPLEX BUS, BUILT IN TEST, F-15 AVIONICS INTERFACE CARD |
| FTLD | FUNCTIONAL DESCRIPTION | F15 SAASM EMBEDDED GPS/INS (EGI) UNIT IS A SELF CONTAINED ALL-ATTITUDE LINE REPLACEABLE NAVIGATION UNIT. POVIDES THE FOLLOWING OUTPUTS: ACCELERATION, ATTITUDE (AZIMUTH, PITCH, ROLL), ATTITUDE RATES AND UNIVERSAL TIME COORDINATED. PROVIDES INERTIAL, BLENDED & GPS ONLY POSITION SOLUTIONS |
| RDAL | REFERENCE DATA AND LITERATURE | DDFORM61 |
| TMDN | TYPE/MODEL DESIGNATION | CN-1689(V)15/ASN |