HARDWARE / PRODUCT

400 mNms Microsatellite Reaction Wheel

Sinclair Interplanetary (Rocket Lab)
400 mNms Microsatellite Reaction Wheel

High-torque, radiation-hardened wheel for high-agility remote sensing or science microsatellites.

Technical specifications

Angular momentum capacity
400 mNms
Equivalent CMG performance
0.4 Nms CMG at 22.5 deg/sec gimbal rate
Target application
High-agility remote sensing / science microsatellites
Design focus
High torque, radiation hardness
Control interface
Digital serial bus, commandable speed/momentum/torque

About

Sinclair Interplanetary pioneered high-reliability vacuum-lubricated reaction wheels for picosatellites, nanosatellites and microsatellites, with a built-in digital processor commandable over a serial bus for speed, momentum or torque, plus digital telemetry on speed, temperature, voltage, current and other health parameters. The 400 mNms Microsatellite Wheel is optimized for torque and radiation hardness. It can deliver performance equivalent to a 0.4 Nms control moment gyro with a 22.5 deg/sec gimbal rate, at much reduced mass and complexity, and is designed for high-agility remote sensing or science microsatellites.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: web.archive.org ↗