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Power Control Assembly (PCA)

Invocon’s Remote Power Control (RPC) Remote Ground Support Equipment (RGSE) provides for power control and monitoring for Avionics or Flight Termination System (FTS) payloads. This includes system monitoring, power switching (e.g., internal/external, on/off), and battery maintenance as well as RS422 communications all through the vehicle’s UMBI(s). The rack is controlled remotely via direct Ethernet connection or through a fiber optic converter for extended range.

Key Specifications

Specification
Value
Input Voltage
22.5 – 33.6 VDC
Output Current (28V channels combined)
12 A
Output Current (5V / 12V auxiliary)
2.0 A
Power Outputs
2x switched 28V, 1x un-switched 28V, 1x auxiliary 5V or 12V
Connectors
D-Sub (Battery, UMBI/Lanyard, Telemetry, Unswitched/Aux, Switched/Status)
Size (L x W x H)
4.85" x 4.4" x 1.4" (excluding connectors)
Weight
1.5 lbs
Case Material
6061 aluminum, Alodine coated
Operating Temperature
-24 to 71°C

Key Features

  • Dropout-Free Internal/External Power Switching

    Designed specifically to prevent power dropouts when transitioning between internal battery and external ground power, protecting sensitive avionics loads.

  • Configurable Auxiliary Output

    5V or 12V auxiliary output configurable for source (switched or un-switched 28V channel) and voltage level to match payload requirements.

  • Over-Voltage Protection

    One switched 28V output includes configurable over-voltage protection for protection of sensitive downstream loads.

  • Standard Sequencing Semantics

    Supports All Fire, No Fire, Power Backup 1, and Power Backup 2 sequencing for compatibility with standard small launch vehicle avionics architectures.

  • Battery Charging Support

    Integrated battery charging support simplifies pre-launch vehicle maintenance by enabling battery top-off without removing the assembly.

  • UMBI/Lanyard Interface

    UMBI and lanyard connections support standard ground handling and launch sequencing operations.

Typical Applications

  • Small Launch Vehicle Avionics Power

    Provides centralized power switching and distribution for all onboard avionics during ground operations and flight.

  • Pre-Launch Battery Maintenance

    Manages battery charging and health monitoring to ensure sufficient mission power prior to launch.

  • Internal/External Power Transition

    Handles the critical umbilical-pull transition from external ground power to internal battery power without interruption.

  • Payload Power Distribution

    Supplies regulated 5V or 12V auxiliary power to payload electronics requiring lower voltage rails.

Available Configurations

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