Spacecraft Mechanisms Actuators & Servoactuators

Type 2 Solar Array Drive Assembly (SADA)

Type 2 Solar Array Drive Assembly

The single axis Type 2 Solar Array Drive Assembly (SADA) is based on the Type 2 Rotary Incremental Actuator. The standard actuator has been produced with numerous design variations to meet mission requirements for many applications. The features that vary are interface parameters and power transfer requirements. All of the listed Type 2 SADA designs are configured with harmonic drive gear sets, potentiometers for position sensing, and a slip ring assembly for power and signal transfer. Key specification parameters for a typical qualified unit are shown in the table below. The Type 2 SADA easily interfaces with the Moog 2 or 4 channel Electronic Control Unit for a complete system solution.

Specifications

  • Output Step Size

    0.02 degrees

  • Output Torque

    11 (Nm)

  • Operating Temperature Range

    -50°C to +80°C

  • Mass

    < 3.50 Kg including harness

  • Holding Torque Powered

    9 Nm

  • Holding Torque Unpowered

    4.5 Nm

  • Inertia Capability

    28 Kg.m2

  • Power Slip Rings

    34 rings @ 3.2 A

  • Signal Slip Rings

    15 rings @ 1.0 A

  • Position Sensor

    Potentiometer ± 0.36°

Our extensive product offering of Solar Array Drive Assemblies are flexible and customizable to your specific needs. For more information on Solar Array Drive Assemblies, or this specific model please contact our Chatsworth facility.

Type 2 SADA Datasheet

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Spacecraft Mechanisms Product Catalog

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For Additional Information Regarding our Spacecraft Products:

Philip Tokeshi

Spacecraft Mechanisms Sales Manager

+1-818-734-6770