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
- SatCatalog_-_Collins_Aerospace_-_RSI_4-75-60_-_Datasheet.pdf PDF source: satcatalog.s3.amazonaws.com ↗
Need the full ICD, test reports or a specific revision? Ask the supplier directly.