Modular Deployment Sequencer (MDS)
The Modular Deployment Sequencer (MDS) is a dual-redundant system that ensures precise satellite deployment by activating upon a valid command from the Launch Vehicle (LV) and executing preprogrammed deployment sequences.
Technical specifications
- Mass
- ~1 kg for four deployers powered from external power up to ~ 2 kg for 8 deployers powered from internal power
- Mass (2)
- ~3.8 kg for 32 deployers powered from high current battery option
- Dimensions
- 250x100 mm base area
- Supply voltage
- 28 V+-4 V
- Pulse Power Supply Duration
- 0.1-2 s
- Activation pulse
- 28 V± 4 V
- Activation pulse duration
- 100 ms
- Activation pulse current
- <100 mA
- No fire activation
- <10 V
- Interface
- Traditional Analog “breakwire” interfaces, RS485, RS422, USART, CAN Bus, Ethernet
- Interface (2)
- USART (optional RS422/RS485 isolation)
- Interface (3)
- CAN
- Interface (4)
- SPI (optional galvanic isolation)
- Interface (5)
- Ethernet over shielded twisted pair
About
The Modular Deployment Sequencer (MDS) is engineered for precision, reliability, and flexibility in satellite deployment. It serves as a crucial interface between launch vehicles and deployer systems, guaranteeing accurate satellite release. The system incorporates dual redundancy to effectively mitigate single-point risks, enhancing mission success. Powered by an internal Lithium-Ion battery, the MDS activates upon receiving a valid command from the Launch Vehicle (LV). Once activated, it executes preprogrammed deployment sequences, signaling deployer systems and their doors. It ensures that satellites deploy at their preset times and collects separation confirmations. This critical data is then relayed back to the LV, providing essential mission assurance. The MDS is designed to be a robust and dependable solution for managing the complex process of satellite deployment.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.