NSN 6605-01-357-8976 · NIIN 013578976 · FSC 6605
NO DASHES 6605013578976
In Stock
INERTIAL NAVIGATION UNIT
Navigational Instruments
Application: INERTIAL NAVIGATION SYSTEM F-16, A-10, FB-111, C-130, RF4C, EF-111 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 |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES NOMINAL 11.780 |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 6.530 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 8.150 |
| ACDC | CURRENT TYPE | AC |
| AGAV | END ITEM IDENTIFICATION | INERTIAL NAVIGATION SYSTEM F-16, A-10, FB-111, C-130, RF4C, EF-111 AIRCRAFT |
| ELEC | VOLTAGE IN VOLTS | 115.0 AND 200.0 |
| FAAZ | PHASE | SINGLE |
| FEAT | SPECIAL FEATURES | MOUNTING: HARD MOUNTED; MATERIAL: ALUMINUM ALLOY CASE; PROVIDES OUTPUTS OF ACCELERATION, VELOCITY, POSITION, HEADING, ATTITUDE (PITCH AND ROLL), ATTITUDE RATES (PITCH, ROLL, AZIMUTH) AND TIME, PITCH AND ROLL SYNCHRO (ANALOG), BARO INERTIAL ALTITUDE (WHEN PROVIDED WITH BAROMETRIC ALTITUDE DATA); PERFORMS RAPID REACTION, SOTRED HEADING ALIGNMENTS, RAPID REACTION ALIGNMENT OF A DEGRADED ACCURACY (ATTITUED HEADING REFERENCE SYSTEM) MODE WITH OUTPUTS OF HEADING, ATTITUDE, ANGULAR RATE AND ACCELERATION |
| FREQ | FREQUENCY IN HERTZ | 400.0 |
| FTLD | FUNCTIONAL DESCRIPTION | PROVIDES A SELF CONTAINED FULLY AUTOMATIC STRAPDOWN INERTIAL REFERENCE FOR PILOTING AND NAVIGATING AN AIRCRAFT |
| NHCF | NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| RDAL | REFERENCE DATA AND LITERATURE | TECH ORDER 5N1-4-23-14 |
Supersedes
This item replaces cancelled NIIN 012319755. An older drawing citing one of those numbers resolves here.