Scheduled Maintenance We will be conducting scheduled maintenance on 4/19 from 10:00 PM EST to 4/20 9:00 PM EST. During this time MyAerospace applications will be temporarily unavailable. We apologize for any inconvenience this may cause.​​
Scheduled Maintenance We will be conducting scheduled maintenance on 4/19 from 10:00 PM EST to 4/20 9:00 PM EST. During this time MyAerospace applications will be temporarily unavailable. We apologize for any inconvenience this may cause.​​
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LASEREF VI Micro Inertial Reference Systems

LASEREF VI Micro Inertial Reference Systems

LASEREF VI inertial reference unit (IRU) offers on-aircraft data load capability, HIGH Step II software for 100% availability of low required navigation performance authorized required (RNP AR) with integrity coasting, automatic dependent surveillance-broadcast (ADS-B) compliance with civil certified global navigation satellite system (GNSS) receiver & automatic mode control with align-in-motion.

LASEREF VI inertial reference unit (IRU) offers on-aircraft data load capability, HIGH Step II software for 100% availability of low required navigation performance authorized required (RNP AR) with integrity coasting, automatic dependent surveillance-broadcast (ADS-B) compliance with civil certified global navigation satellite system (GNSS) receiver & automatic mode control with align-in-motion.

Our LASEREF VI is the smallest, lightest and lowest power IRU on the market. It is one-half-the-size, one-third-the-weight and requires one-third-the-power than the LASEREF IV. The system is available for rotorcraft and fixed-wing applications.

Other key elements include:

  • Automatic mode control logic and initialization
  • Optimal sensor performance to provide the best performance for high bandwidth SATCOM (e.g. JETWAVE SATCOM), SVS (Synthetic Vision System), CVS (Combined Vision System), and HUD (Heads Up Display)
  • Meets both fixed wing and rotary wing environmental and electromagnetic environments
  • Passively cooled - avoiding cost and space for cooling fans
  • On-aircraft data load capability
  • Honeywell's inertial GPS hybrid (HIGH) integrity coasting provides 100% availability of RNP AR navigation and can eliminate predictive receiver autonomous integrity monitoring (RAIM) for non-precision GPS approaches
  • Installation configurable features such as lever arm compensations and selectable output filtering eases integration and installation into existing aircraft

Brochures  (2)
Brochures  (2)
Laseref VI for Helicopters
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Laseref VI Micro Inertial Reference System
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Datasheet  (1)
Datasheet  (1)
Laseref VI
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Segment OEM Platform Product
DS Airbus Helos   LR6
DS Agusta AW-1X9 LR6
AT Boeing 787 LR6 (BC02)
AT Boeing 777X LR6 (BC02)
AT Bombardier CRJ-1000 LR6 (BC02)
AT Bombardier Cseries LR6 (BC02)
RT Bombardier Q400 LR6 (BCxx)
BA Bombardier C350 LR6 (BCxx)
BA Bombardier CL6 LR6 (BCxx)
BA Bombardier G5000E LR6 (BCxx)
BA Bombardier G7000/8000 LR6 (BCxx)
DS C-295   LR6
BA Cessna Lat/Long/LR LR6 (BCxx)
AT COMAC C919 LR6 (BCxx)
BA Dassault F2000 LR6 (BCxx)
BA Dassault F6X, F10X LR6 (BCxx)
AT Embraer E2 LR6 (BCxx)
BA Gulfstream G450 LR6 (BCxx)
BA Gulfstream G550 LR6 (BCxx)
BA Gulfstream G650 LR6 (BCxx)
BA Gulfstream G500 LR6 (BCxx)
BA Gulfstream G600 LR6 (BCxx)
BA Gulfstream G650/G700/G800 LR6 (BCxx)
BA Gulfstream G500/G600 LR6 (BCxx)
AT Irkut MS-21 LR6 (BCxx)
AT Mitsubishi MRJ LR6 (BCxx)
BA Pilatus PC-21, 24 LR6
BA Syberjet SJ30-2 LR5/LR6