PA-RR-260-8-C-24-C-315-00 redundant rotary servo actuator

PA-RR-260-8-C-24-C-315-00 is a redundant rotary servo actuator with dual brushless motors and independent control channels. Its RS485 interface commands shaft positioning, while internal fault handling transfers operation to the backup drive.
Description
The PA-RR-260-8-C-24-C-315-00 is a redundant rotary servo actuator from Pegasus Actuators, designed for safety-critical unmanned aircraft and other unmanned systems that use control surfaces or levers driven through a rotating output shaft. It combines two brushless motors, two servo controllers and three contactless angle sensors in a single housing.
The redundancy is handled inside the actuator. Multiple master control units reach a majority decision, and after a motor, power stage or signal-cable fault the second channel takes over without any action from the autopilot. The autopilot only receives a warning signal. In normal operation the first motor and its power stage work, and the second is engaged after the first has failed. Pegasus states that the actuator keeps its full torque, speed and bandwidth after a single failure. The only requirement on the host is two identical command channels.
The main figures are as follows. Continuous torque is 300 Ncm and stall torque is 500 Ncm or more, with the slip clutch releasing between 500 and 600 Ncm to protect the gear train and the airframe. No-load speed is 210 deg/s at 24 V, and speed at rated torque is 135 deg/s typical. The travel angle is 315 deg with a magnetic redundant contactless angle sensor. Gear train backlash is at most 0.5 deg, and the weight is 480 g typical. Axial load on the output shaft must stay below 100 N and lateral load below 300 N.
For power, the operating range is 18 to 32 V with 24 V typical, and the absolute maximum is 34 V. At 24 V the standby current is typically 130 mA with both channels connected, and the operating current is typically 500 mA against a 300 Ncm load. Each channel needs its own power input.
The command interface is RS485 with a redundant data protocol, with baud rates from 9600 to 230400 bit/s and 115200 typical, and a switchable termination resistor built in. CANopen CiA 402 is listed as an option under a different order code. The actuator uses two Glenair Series 801 Mighty Mouse 7-pin connectors, and the aluminium case has a solid 4-point fixation. Installation frames, levers and programming tools such as PA-Control 3 are offered as accessories.
The case is protected to IP67 against water and dust, the operating temperature range is -40 to +70 degrees C, and the environmental conditions are designed to comply with DO-160 F and MIL-STD-810.
Typical applications are primary flight control surfaces, swashplate and lever-driven linkages on unmanned aircraft where a single actuator fault must not cause a loss of control.
Specifications
| General | |
|---|---|
| Grade | Professional[1] |
| Market | Dual-use |
| Platform class | Large UAS (25–150 kg), Heavy UAS (>150 kg), eVTOL |
| Airframe | Fixed-wing, Helicopter, Tiltrotor/tiltwing, Hybrid VTOL |
| Availability | In production |
| Mass | 480 g[1] |
| Operating temperature | -40 – 70 °C[1][2] |
| Waterproofness (IP rating) | IP67[1] |
| Key specifications | |
| Speed | 210 °/s[1] |
| Rotation range | 315 °[1] |
| Supply voltage | 18 – 32 V[1][2] |
| Physical interfaces | RS-485[1] |
| Additional specifications | |
| Stall torque | 5 Nm[1][2] |
| Backlash | 0.5 °[1][2] |
| Gear material | Hardened steel spur gears.[1][2] |
| Redundancy | Dual[1] |
| Certifications and compliance | |
| Certifications | IP67 |
Sources
- pegasus-actuators.com/product/redundant-actuator/pa-rr-260-8.html · checked October 25, 2026
- pegasus-actuators.com/fileadmin/user_upload/products/redundant/RR260-8/Datasheet-RR260-8-C-24-C-315-00_A05.pdf · checked October 25, 2026
A value without a number has no recorded source yet: we are adding it.
Frequently asked questions
What is the primary purpose of the PA-RR-260-8 redundant servo-actuator?
The PA-RR-260-8 is designed for safety-critical unmanned systems to enhance servo-actuator reliability.
How does the actuator handle redundancy-related decisions?
All decisions regarding redundancy are processed internally by the actuator itself.
What happens to the actuator's performance if a single point failure occurs?
The actuator maintains its full torque, rotational speed, and bandwidth even after a single point failure.
What are the physical and electrical specifications of the PA-RR-260-8?
The actuator operates at 24 V DC, weighs 480 grams, and provides a continuous torque of 300 Ncm.
What is the travel angle of the PA-RR-260-8?
The travel angle of the actuator is 315 degrees.
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