Inertial Measurement Unit — Booster Rate Gyro

BoRG

A mission-critical inertial sensing solution engineered for the demanding flight-control requirements of commercial space launch vehicles — delivering precise pitch and yaw rate data from pre-launch through booster engine cutoff and stage separation.

±80°/s rate range  ·  Triple-redundant channels  ·  ±10°/hr bias stability
≥ ±80°/s
Rate Input Range
≤ ±10°/hr
Bias Stability
Triple
Redundant Channels
16.5 lb
Weight
24–34 VDC
Power Input
BoRG Booster Rate Gyro Inertial Measurement Unit
The Hardware

One triple-redundant unit

The BoRG pairs precision rate sensing with a fully redundant triple-channel architecture — isolated sensing, power, and communication paths keep the unit operating through harsh aerospace launch environments. High-speed Ethernet and a redundant aerospace-grade bus deliver robust real-time data to the flight computer, while onboard processing handles all sampling, filtering, and buffering for low-latency performance.

Triple Redundancy High-Speed Ethernet Aerospace-Grade Reliability
Key Performance Features

Precision built for launch

Engineered for maximum reliability, the BoRG delivers accurate, low-latency performance for mission-critical launch applications where precision, redundancy, and reliability are essential.

Precision Sensing

  • Precision rate sensing
  • High bias stability
  • Low noise performance
  • Precision alignment

Redundancy & Reliability

  • Triple redundancy
  • Fault-tolerant design
  • Aerospace-grade reliability
  • Ruggedized architecture

Real-Time Performance

  • Low latency
  • Real-time processing
  • Wide dynamic range
  • High-speed Ethernet
Mission Profile

From pad to stage separation

Stable, accurate vehicle guidance across every phase of ascent — precise pitch and yaw rate data enables continuous, reliable control from pre-launch through booster engine cutoff and stage separation.

Pre-Launch

  • Vehicle checkout & alignment
  • Precision rate zeroing

Powered Ascent

  • Pitch & yaw rate sensing
  • Booster engine cutoff guidance

Stage Separation

  • Real-time attitude data
  • Seamless handoff to upper stage
Background

75 years of inertial heritage

Aerosphere Power & Navigation (APN), located in Budd Lake, NJ, has been designing, developing, and producing inertial components, sensors, and navigation systems for Space, Ground, and Avionic applications for over 75 years. APN has been developing closed-loop Fiber Optic Gyros (FOGs) and Ring Laser Gyros (RLGs) since the early 1990s, producing and delivering IMU products with performance ranging from tactical to strategic grade.

Documentation

Technical specifications

01Performance+
Rate Input Range≥ ±80°/s
Resolution≤ 0.006°/s
Scale Factor Accuracy≤ 6000 PPM or ≤ 0.02°/s
Bias Stability≤ ±10°/hr
Angular Random Walk≤ ±1°/√hr
Bias Repeatability≤ ±5°/hr
Turn-On Bias Error≤ ±720°/h
02Interfaces & Architecture+
CommunicationsHigh-Speed Ethernet
Redundant CommunicationsAerospace-Grade Redundant Bus
ArchitectureTriple-Redundant Channels
Data ProcessingIntegrated Sampling, Filtering & Buffering
03Physical+
Weight16.5 lb
Dimensions13.25" × 9.5" × 5.6"
Power Input24 to 34 VDC
PDF
BoRG Datasheet
Full performance and interface specifications
Download
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sensing engineer

From datasheet questions to evaluation units, our team can help scope BoRG for your launch vehicle.