NSN 6605-01-357-8976
Part Details | INERTIAL NAVIGATION UNIT
6605-01-357-8976 A self-contained Line Replaceable Unit that provides acceleration, velocity, and position data for land vehicles, watercraft or aircraft. It may also provide altitude information for aircraft. It is part of an INERTIAL NAVIGATION SYSTEM and may contain an INERTIAL REFERENCE UNIT, NAVIGATION.
Alternate Parts: 983533610, 9835336-10, 9835336, SNU 841, SNU 84-1, CN1656ASN, CN-1656/ASN, AF AVIONICS SP IL, AF AVIONICS S/P IL, 89050011, 890500-11, 8905000011, 890500-0011, 6605-01-357-8976, 01-357-8976, 6605013578976, 013578976
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | MAY 05, 1992 | 01-357-8976 | 53294 ( INERTIAL NAVIGATION UNIT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6605-01-357-8976
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9835336-10 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
| 9835336 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
| SNU 84-1 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
| CN-1656/ASN | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
| AF AVIONICS S/P IL | 1HBK1 | MIL-HDBK-300HQ AFMC-LGIS |
| 890500-11 | 06481 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
| 890500-0011 | 06481 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NAVIGATION AND MARITIME SYSTEMS |
Technical Data | NSN 6605-01-357-8976
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 11.780 INCHES NOMINAL |
| OVERALL WIDTH | 8.150 INCHES NOMINAL |
| OVERALL HEIGHT | 6.530 INCHES NOMINAL |
| CURRENT TYPE | AC |
| VOLTAGE IN VOLTS | B115.0$$B200.0 |
| FREQUENCY IN HERTZ | 400.0 |
| PHASE | SINGLE |
| 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 |
| NUCLEAR HARDNESS CRITICAL FEATURE | HARDENED |
| FUNCTIONAL DESCRIPTION | PROVIDES A SELF CONTAINED FULLY AUTOMATIC STRAPDOWN INERTIAL REFERENCE FOR PILOTING AND NAVIGATING AN AIRCRAFT |
| REFERENCE DATA AND LITERATURE | TECH ORDER 5N1-4-23-14 |
| END ITEM IDENTIFICATION | INERTIAL NAVIGATION SYSTEM F-16, A-10, FB-111, C-130, RF4C, EF-111 AIRCRAFT |
