HARDWARE / PRODUCTUpdated 24 Jul 2026

Reaction Wheels

Sinclair Interplanetary (Rocket Lab)
Reaction Wheels

Sinclair Interplanetary offers a range of high-reliability, vacuum-lubricated reaction wheels for picosatellites, nanosatellites, and microsatellites, featuring built-in digital processors for precise control and telemetry.

Typed specifications41 values

Discloses 7 of 10 fields engineers filter by in this category (category median 5).

Mass
120 g
datasheet p.1
Envelope (L×W×H)
50 mm x 50 mm x 30 mm
datasheet p.1
Angular momentum storage
0.01 N·m·s
Nominal · datasheet p.1 0.018 N·m·s peak, at 5 V supply  |  0.018 N·m·s max · peak (at 5 V supply)  |  0.01 N·m·s nom. · nominal
Max torque
1 mN·m
±1 mNm at 0.01 Nms (at 5 V supply) · datasheet p.1 1 mN·m at 0.01 Nms (at 5 V supply)
Supply voltage
3.4 V
min · Nominal · datasheet p.1 8 V max · Maximum  |  6 V max · Nominal  |  3.4–6 V nominal  |  3.4–6 V nom. · Nominal
Power consumption
0.11 W
@ 0.005 Nms, steady state · datasheet p.1 1.05 W @ 0.01 Nms, + 1 mNm  |  0.25 W @ 0.018 Nms, steady state  |  0.11 W 0.005 Nms, steady state (in vacuum)  |  1.05 W 0.01 Nms, + 1 mNm (in vacuum)  +1
Data interface
UART
datasheet p.1 I2C I2C/SMBus  |  other SMBus  |  I2C
Operating temperature
-40 °C
min · datasheet p.1 70 °C max  |  -40–70 °C operating
Radiation tolerance (TID)
20 krad
datasheet p.1 20 krad min · >20 krad dose
Design lifetime
10 years
on-orbit · datasheet p.1
Wheels in the unit
1
datasheet p.0
Bearing type
ball
Diamond coated hybrid ball bearings · datasheet p.1
Random vibration
12 g RMS
min · >12 gRMS · datasheet p.1
Flight heritage
10 Units total on-orbit on 4 satellites, first launched June 2014
datasheet p.1
Satellite class
CubeSat
datasheet p.0
Missions flown
10
units total on-orbit on 4 satellites · datasheet p.1
Drive electronics
integrated
built-in control CPU · datasheet p.1
Volume
0.25 U
datasheet p.1
Control modes
speed
datasheet p.1 torque
Indicative price
20 000 EUR
each; +US$2000 for radiation lot-screened parts · datasheet p.1 18 400 EUR each; converted from USD at 0.92

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier19 lines, in the manufacturer's own wording
1 nms microsatellite wheel suitability
100 kg Earth-observation missions
1 nms microsatellite wheel units on-orbit
76 units on 19 spacecraft
1 nms microsatellite wheel first launch
June 2016
1 nms GEO wheel features
Hardened version of heritage 1 Nms wheel, rad-hard parts, shielded enclosure, active mechanism to mitigate deep charging, greatly reduced power consumption
1 nms GEO wheel suitability
High orbits
1 nms GEO wheel first flight deliveries
Q1 2020
400 mnms microsatellite wheel optimization
Torque and radiation hardness
400 mnms microsatellite wheel performance equivalent
0.4 Nms CMG with 22.5 deg/sec gimbal rate
400 mnms microsatellite wheel design for
High-agility remote sensing or science microsatellites
60 mnms microsatellite wheel features
High-torque motor phase current control electronics in a small package
60 mnms microsatellite wheel units on-orbit
68 units on 20 spacecraft
60 mnms microsatellite wheel first launch
June 2014
30 mnms nanosatellite wheel first launch
April 2008
30 mnms nanosatellite wheel units on-orbit
61 units
30 mnms nanosatellite wheel fit
6U to 12U cubesat
10 mnms picosatellite wheel suitability
Smaller cubesats
10 mnms picosatellite wheel units on-orbit
10 units on 4 spacecraft
10 mnms picosatellite wheel first launch
June 2014
3 mnms picosatellite wheel capacity
3 wheels in a 1U Cubesat, 4-wheel pyramid configuration possible

About

Sinclair Interplanetary pioneered high-reliability vacuum-lubricated reaction wheels for picosatellites, nanosatellites, and microsats. There are currently 76 wheels on-orbit, all working well. All of these reaction wheels incorporate a built-in digital processor. They can be commanded over a serial bus to produce a desired speed, momentum, or torque. They report digital telemetry concerning speed, temperature, voltage, current, and other health parameters. The product line includes several models:

1 Nms Microsatellite Wheel: This is the largest wheel, suitable for 100 kg Earth-observation missions. There are currently 76 units on-orbit on 19 spacecraft, with the first launch in June 2016.

1 Nms GEO Wheel: This is a hardened version of the heritage 1 Nms wheel, suitable for high orbits. It uses rad-hard parts, has a shielded enclosure, and employs an active mechanism to mitigate deep charging of the rotor assembly. Power consumption is greatly reduced. First flight deliveries are scheduled for Q1 2020.

400 mNms Microsatellite Wheel: This wheel is optimized for torque and for radiation hardness. It can give performance equivalent to a 0.4 Nms CMG with 22.5 deg/sec gimbal rate at much reduced mass and complexity. Designed for high-agility remote sensing or science microsatellites.

60 mNms Microsatellite Wheel: This wheel packs high-torque motor phase current control electronics into a small package. There are 68 units on-orbit on 20 spacecraft, with the first launch in June 2014.

30 mNms Nanosatellite Wheel: This was the first wheel design and remains the most popular. First launched in April 2008, there are now 61 units on-orbit. Many of these are onboard the University of Toronto SpaceFlight Lab’s GNB series of spacecraft. They fit comfortably into a 6U to 12U cubesat.

10 mNms Picosatellite Wheel: This wheel is ideally suited for smaller cubesats. There are 10 units on-orbit on 4 spacecraft, with the first launch in June 2014.

3 mNms Picosatellite Wheel: This wheel is so tiny that 3 wheels can be carried in a 1U Cubesat. A 4-wheel pyramid configuration is also possible.

Documentation

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

Source: web.archive.org ↗

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