NSN 6605-01-532-6515
Part Details | INERTIAL NAVIGATION SYSTEM
6605-01-532-6515 A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw and roll axis of land vehicle, watercraft or aircraft and calculates the distance from a reference point. They can include INERTIAL NAVIGATION UNIT(s); PLATFORM, INERTIAL; power supplies; subsystems; mode selectors; and control displays.
Alternate Parts: 34249950R004960, 34249950-R004-960, CN1689(V)16ASN, CN-1689(V)16/ASN, 6605-01-532-6515, 01-532-6515, 6605015326515, 015326515
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | AUG 15, 2005 | 01-532-6515 | 53295 ( INERTIAL NAVIGATION SYSTEM ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6605-01-532-6515
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 34249950-R004-960 | 0BFA5 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| CN-1689(V)16/ASN | 80058 | JOINT ELECTRONICS TYPE DESIGNATIONSYSTEM |
Technical Data | NSN 6605-01-532-6515
| Characteristic | Specifications |
|---|---|
| OVERALL WIDTH | 8.500 INCHES NOMINAL |
| OVERALL HEIGHT | 11.000 INCHES NOMINAL |
| SPECIAL FEATURES | A) PROVIDES OUTPUTS OF: ACCELERATION, VELOCITY, POSITION, HEADING B) CONTAINS 3-RING LASER GYROS AND 3 ACCELEROMETERS IN A STRAPDOWN CONFIGURATION C) EMBEDDED GLOBAL POSITIONING SYSTEM RECEIVER (EGR) (RF INPUT) - GASR BASED. D) 1553/B MULTIPLEX BUS COMPATIBLE E) BUILT IN TEST INCORPORATED F) 32 BIT MICROPROCESSOR G) MULTI-MODE RECEIVER THAT PROVIDES: INSTRUMENT LANDING SYSTEM (ILS), VERY HIGH OMNI BEARING RECEIVER (VOR), MARKER BEACON (MB) |
| FUNCTIONAL DESCRIPTION | THE P3I EMBEDDED GPS/INS (EGI)+ WITH MULTI MODE RECEIVER (MMR) UNIT IS A SELF- CONTAINED ALL ATTITUDE NAVAGATION 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) SYCHRONIZED TIME VIA EXTERNALLY CONTROLLED MIL-STD-1553B DUAL MULTIPLEX DATA BUS WHICH RECEIVES DATA AND TRANSMITS UPDATED DATA BASED THE REQUIREMENTS OF THE INTERFACING AVIONICS SYSTEMS. THE MMR PROVIDES FOR A PROTECTED INSTRUMENT LANDING SYSTEM (P-ILS), A VERY HIGH OMNI BEARING RECEIVER (VOR), AND A MARKER BEACON (MB) FUNCTIONALITY. THE EGI+ W/MMR PROVIDES SIMULTANEOUS INERTIAL, BLENDED AND GPS ONLY POSITION SOLUTIONS. IT INCORPORATES A GSAR BASED RECEIVER. |
| END ITEM IDENTIFICATION | CN-1689 |
