HARDWARE / PRODUCTAdded 23 Jul 2026

RSI 4-75/60 Momentum and Reaction Wheel

Collins Aerospace
RSI 4-75/60 Momentum and Reaction Wheel

Compact TELDIX momentum/reaction wheel with integrated wheel drive electronics for small satellite attitude control, 0.04-4 Nms class.

Typed specifications29 values

Discloses 6 of 10 fields engineers filter by in this category (category median 5).

Mass
3 700 g
max · datasheet p.2
Envelope (L×W×H)
diameter 222 mm, height 85 mm
datasheet p.2 222 mm x 85 mm Diameter x Height
Angular momentum storage
4 N·m·s
at nominal speed · datasheet p.2
Max torque
75 mN·m
at nominal speed · datasheet p.2 75 mN·m motor torque at nominal speed
Speed range
-6 000–6 000 rpm
operational speed range +/- 6,000 rpm · datasheet p.2
Supply voltage
24 V
min · datasheet p.2 51 V max  |  24–51 V
Power consumption
90 W
max · Maximum torque at nominal speed · datasheet p.2 20 W max · Steady state at nominal speed
Operating temperature
-5–50 °C
mineral oil · datasheet p.2 -20–70 °C synthetic oil  |  -5–50 °C mineral oil  |  -20–70 °C synthetic oil
Design lifetime
15 years
>, in orbit · datasheet p.3 15 years in orbit  |  15 years min · in orbit
Peak power
90 W
max · maximum torque at nominal speed · datasheet p.2
Survival temperature
-20–60 °C
mineral oil · datasheet p.2 -40–75 °C synthetic oil
Flight heritage
Part of TELDIX wheel family with 40+ years heritage, 7,300+ cumulative in-orbit years
product page
Satellite class
smallsat 100-500 kg
for satellites weighing 200 - 1,000 kg · datasheet p.1 microsat 10-100 kg for satellites weighing 200 – 1,000 kg  |  large >500 kg for satellites weighing 200 - 1,000 kg  |  smallsat 100-500 kg for satellites weighing 200 – 1,000 kg  |  large >500 kg for satellites weighing 200 – 1,000 kg
Drive electronics
integrated
with integrated Wheel Drive Electronics · datasheet p.1

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 supplier22 lines, in the manufacturer's own wording
Mass
3.7 kg
Power
20.0 W average
Interface
Form factor: SmallSat
Flight heritage
Part of TELDIX wheel family with 40+ years heritage, 7,300+ cumulative in-orbit years
TRL
9 (flight-proven)
Momentum
4 Nms
Operating speed range
± 6,000 rpm
Speed limiter (EMF)
< 7,000 rpm
Torque
75 mNm
Loss torque
< 20 mNm
Diameter
222 mm
Height
85 mm
Power consumption (Steady state at nominal speed)
< 20 W
Power consumption (Maximum torque at nominal speed)
< 90 W
Supply voltage
24 to 51 VDC
Input current
< 3.75 A
Qualification/protoflight temperature (mineral oil)
-10 to +55 °C
Qualification/protoflight temperature (synthetic oil)
-25 to +75 °C
Operating temperature (mineral oil)
-5 to +50 °C
Operating temperature (synthetic oil)
-20 to +70 °C
Survival/Non-operating Temperature (mineral oil)
-20 to +60 °C
Survival/Non-operating Temperature (synthetic oil)
-40 to +75 °C

About

The RSI 4-75/60 is the smallest wheel in Collins Aerospace’s TELDIX space wheel family, delivering angular momentum storage in the sub-4 Nms range with fully integrated Wheel Drive Electronics (WDE). It provides attitude control and momentum/reaction wheel functionality for small spacecraft starting around 30 kg, and shares the same hermetic sealing, modular configuration, and power/loss-torque optimization design philosophy as the rest of the TELDIX line, which has accumulated more than 40 years of product heritage and 7,300+ cumulative years of in-orbit operation across the wheel family. It is currently in production and flight-proven.

Documentation

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

Source: www.collinsaerospace.com ↗

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