LR-450 Inertial Measurement Unit (IMU)

AVAILABLE, FALL 2024

satellite hovering over earth

High Performance Space IMU

Introducing the LR-450 — the new standard for long-life and high-performance space missions, as an alternative to first-generation ring laser gyroscopes (RLG). Measuring just 341 cubic-inches, weighing under 10 pounds and requiring less than 15 watts of power, the LR-450 is well suited for mid-size satellite and deep space applications.

The LR-450 incorporates Northrop Grumman’s milli-HRG™ (mHRG™) Precision Space Gyroscope, which uses the same critical quartz components — high-Q resonator and inner electrode assembly — employed in Northrop Grumman’s proven hemispherical resonator gyroscope (HRG) technology. The HRG has achieved more than 70 million error-free hours in space missions.

A single LR-450 can take the place of two RLG IMUs, optimizing SWaP-C for a typical 15-year mission.

Learn More > LR-450 Inertial Measurement Unit (IMU) - Datasheet
inertial measurement unit

LR-450 Description

The mHRG™, known for its unmatched reliability in commercial, government and civil space missions, is inherently stable, with no wear-out mechanism, and has high tolerance to radiation effects.

LR-450 configurations include:

  • Three mHRGs™. The inertial instruments are arranged as an orthonormal set
  • Single integrated interface to power supply, communications bus, digital processor and control electronics
  • Optional – a fourth gyro
  • Optional – a set of three accelerometers
space gyroscope inertial measurement unit

LR-450 Applications

The LR-450 is ideally suited for pointing, stabilization and platform attitude control applications, including:

  • Deep space missions
  • Planetary missions
  • Orbital missions, including GEO, MEO and LEO at all inclinations

LR-450 Advantages

The LR-450 provides customers with a robust and high-reliability system.

  • Supports 1553, RS-422 and Ethernet protocols for easy integration into new and existing platforms
  • Stable, low-noise gyros with no wear-out mechanism
  • Inherent radiation hardness of mHRG™, along with spacehardened and high-reliability components
  • Designed for 15-year lifetime
  • Components proven in the HRG, with more than 70 million error-free hours of operation in space

Family of Inertial Measurement Units (IMU) and Navigators

fleet of ships on water

Assured Positioning, Navigation and Timing (PNT)

two-axis gyroscope next to penny

G-2000 Gyroscope Inertial Product Family

military helicopter in flight

LN-200 FOG Family Advanced Airborne IMU/AHRS

LN-200S Inertial Measurement Unit

LN-200S and LN-200HPS Inertial Measurement Units

Two E-2D Advanced Hawkeye aircrafr inflight

LN-251 Advanced Airborne INS/GPS (EGI)

Three-dimensional, multi-mode, gallium nitride radar

LN-270 Pointing, Locating, Navigation and Stabilization System INS/GPS (EGI)

photo of gyro sensor overlayed on globe and space image

Scalable Space Inertial Reference Unit (SSIRU™) Family of Products

In the News

man performing pre-flight preparations aboard military plane

Northrop Grumman’s New Airborne Navigation System Achieves Successful Flight Test

spacecraft in cleanroom

Northrop Grumman Space Navigation Systems Achieve Galactic Threshold – and Keep on Going

satellite, ship, tank illustration

Northrop Grumman’s LEO Satellite Payload for DARPA Revolutionizes Positioning, Navigation and Timing

Contact Us

Eric Scott
eric.scott@ngc.com
(224) 200-7539