LASEREF IV Inertial Reference Systems
Overview
Our LASEREF IV inertial reference system is an all-digital ring laser gyro based inertial reference system providing ARINC 429 and aircraft standard communication bus digital outputs.
- Uses the industry standard GG1320 digital gyro
- 35 percent weight and power reductions versus the LASEREF III
- Lowest cost of ownership with higher reliability and improved maintenance
- Save up to $50K per the HSB when you trade in your old LASEREF II or IIIs
- Automatic re-align function for post flight alignment for quick turns
- Auto-calibration of the sensors to maintain optimal performance over time
- High latitude alignment up to 78.25 degree north latitude
- High latitude magnetic heading map
- Improved maintenance with modular design and assembly
- Interfaces with Honeywell's HG2021 GNSSU ARINC 743A receiver to provide optimal GPS/inertial hybrid computations
- Interchangeable with LASEREF III
- Adapter Tray available for aircraft equipped with Laseref II
- Simple replacement solution for Laseref II and Laseref III
Specifications
Key Differentiators
Features & Benefits
- 10 pounds lighter than LASEREF III
- 25 pounds lighter than LASEREF II
- 30 percent improvement in demonstrated reliability
- Auto-calibration of the sensors to maintain optimal performance over time
- Automatic re-align function for post-flights alignments especially suited for quick turns
- Avionics Maintenance and Service plans are available
- Capable of being updated to latest magnetic variation tables to maintain IFR precision
- High-latitude alignment up to 78.25 degree North latitude
- High-latitude magnetic heading map
- Improved cost of maintenance with a modular design and assembly Interchangeable with LASEREF II (using adapter tray) and LASEREF III (no adapter tray required)
- Interfaces with Honeywell’s HG2021 GNSSU ARINC 743A receiver to provide optimal GPS/ inertial hybrid computations Benefits MTBF (Mean Time Between Failures) consistently exceeds 40,000 hours
- MTBUR (Mean Time Between Unscheduled Removals) more than 20,000 hours since service entry in 1997
- Minimal downtime
- Provides ARINC 429 and aircraft standard communication bus digital outputs
- Uses the industry standard GG1320 digital gyro
Key Savings
- 35% weight and power reductions versus the LASEREF III
- > 30% improvement in reliability with demonstrated >30,000 FH MTBF
Dimensions
Weight
- 25 lbs
- Lighter than LASEREF II and III
Performance Data
Usually Bought With
- Adapter Tray available for aircraft equipped with Laseref II
Software
- HG2001GD15
Replaces
- LASEREF II
- LASEREF III
- Laseref II & III
Receiver
- Interfaces with Honeywell’s HG2021 GNSSU ARINC 743A receiver to provide optimal GPS/ inertial hybrid computations
Mean Time Between Unscheduled Removals (MTBUR)
- More than 20,000 hours since service entry in 1997
Mean Time Between Failures (MTBF)
- 30,000 FH MTBF
- > 40,000 hours
Gyro sensor technology
- GG1320 digital gyro
Components
- HG2001GD03, or Laseref IV with ASCB-C interface HG2001GD15, or Laseref IV with ASCB-A/B interface HG2001GD40 Laseref IV with ASCB-C interface -
Compatible Platform
- BAE Hawker 1000
- BAE Hawker 800
- BAE Hawker 800, 800XP (BAE 125)
- Bombardier
- Bombardier CL-600/601-3A / 3R
- Bombardier CL-600/601-3A/3R
- Bombardier Global Express
- Cessna Citation X
- Dassault F2000
- Dassault F50
- Dassault F900A/B
- Dassault F900C/EX
- Gulfstream G-IV/sp
- Gulfstream G-V
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