Common Space Vehicle Mechanisms

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Actuators at a Glance

Northrop Grumman has been delivering space mechanisms for stowing and articulating spacecraft payloads and solar arrays for 40+ years with 100% mission success and our modular actuators are represented on over 50 missions.

Our designs specialize in:

  • Long-life or high-use missions
  • Low disturbance (induced vibrations reduced for simultaneous operation of payloads)
  • Precision pointing (higher altitude missions)
Data Sheet: Common Space Vehicle Mechanisms

Heritage Products

Deployment Actuators (TRL 9)

Mechanisms to deploy structure or to spool cables. High torque output with current limit drive, or stepper motor (or micro-stepping for low disturbance).

  • Continuous rotation
  • Cable winder mechanisms have two assemblies:
    • Cable Drive Module (CDM)
    • Current Limiter Assembly (CLA)

Solar Array Drive Assembly (TRL 9)

Provides transmission of solar power and electronic signals between solar array and spacecraft; custom or modular slip ring designs for full 360-degree rotation or cable wrap design for limited angle rotations; EMI shielding; Electrically redundant

  • SADA with limited travel (cable management system)
    • Provides bi-directional rotation to maintain limited angle positioning of the solar array
    • Provides absolute angular position knowledge
  • SADA with continuous rotation (slip ring)
    • Provides continual 360-degree rotation of the solar array to maintain solar orientation
    • Provides null position information (via switch ring 1X/Rev)
  • Configurable items:
    • Modular Slip ring - scalable power with 20 or 30 ring modules; Up to four modules (max 120 circuits)
    • Position Feedback: Switch Ring/Poten
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