NSN 6605-01-532-6515 · NIIN 015326515 · FSC 6605
NO DASHES 6605015326515
In Stock
INERTIAL NAVIGATION SYSTEM
Navigational Instruments
Application: CN-1689
Technical characteristics
5 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 |
|---|---|---|
| ABMK | OVERALL WIDTH | INCHES NOMINAL 8.500 |
| ABKW | OVERALL HEIGHT | INCHES NOMINAL 11.000 |
| FEAT | 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) |
| AGAV | END ITEM IDENTIFICATION | CN-1689 |
| FTLD | 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. |
Cross-references
3 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
| Manufacturer part number | CAGE |
|---|---|
| CN-1689(V)16/ASN | 80058 |
| 34249950-R004-002 | 0BFA5 |
| 34249950-R004-960 | 0BFA5 |