• Modular & Scalable Design: Tailored for Mega to smaller missions and deployer systems
  • Reliability Assured: Dual/triple redundant activation and telemetry feedback ensure mission success
  • Multi-Vehicle Compatibility: Qualified for Dnepr, PSLV, Soyuz, Falcon 9, Vega, and more
  • Versatile Power Options: Internal or external power configurations available
modular deployment sequencer
Dual/triple redundant activation
Traditional Analog “breakwire” interfaces
Allows direct monitoring

Product Specification

Mass

~1kg for four deployers powered from external power up to
~ 2kg for 8 deployers powered from internal power
~3.8 kg for 32 deployers powered from high current battery option

Volume

250x100mm base area (height dependent on no. of modules)

Pulse Power Supply

28V+-4V

Pulse Power Supply Duration

0.1-2s

Activation Pulse Characteristics

– Purely resistive load with galvanic isolation to internal circuitry
– Serial switch action with separate ARM and activate pulses.
– Dual redundant pulse switches
– Typical Activation pulse 28V± 4V of 100ms (<100mA)
– “No fire” activation <10V for continuity testing

RF Characteristics

Meets EMI/EMC standards per launch vehicle payload user guides

Digital Interface

Traditional Analog “breakwire” interfaces, RS485, RS422, USART, CAN Bus, Ethernet

LV Telemetry Interface

Direct monitoring: Wire Route physical switches
– Always active
Controlled by sequencer electronics:
1. Galvanically isolated breakwire switches for deployer state change
2. Data bus options: Telemetry feedback or host-commanded deployment
• USART (optional RS422/RS485 isolation)
• CAN
• SPI (optional galvanic isolation)
• Ethernet over shielded twisted pair

Qualification and Acceptance Testing

QT

Is performed on the design/qualification model

AT

Is performed on the unit to be shipped

Functional Test Checked Checked
Thermal Cycling Checked Checked
Thermal Vacuum Unchecked Unchecked
Vibration Test Checked Checked
Mechanical Shock Test Unchecked Unchecked
25
Launched

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