Electro-Explosive System (EES) used for the remote safe ignition of pyrotechnical chains like the ignition of solid rocket motors. MIL-STD-1576 and ECSS-E-ST-33-11C for the design of electro-explosive and pyrotechnical device. ECSS-E-ST-33-01C and ECSS-E-ST-20C for mechanisms and electronic board design.

Features-
•	A safe and arm device (SAD), a mechanism that implements the physical separation between the pyrotechnical component and the pyro-duct.
•	Electronic boards that handle the user-interface and actuate the requested maneuvers.
•	An EED, the pyrotechnical component that generates the SRM ignition.
•	Remove-Before-Flight and Insert-Before Flight devices to provide safety during ground handling.
•	Impossibility to arm the device with only one command.
•	Physical separation between the circuit that circuit that triggers EED and the rest of the electronics.
•	Inhibit monitoring
•	Three electronic inhibits to prevent inadvertent EED ignition
•	Two mechanical inhibits to prevent SAD arming.
•	Space-grade field- programmable gate array (FPGA) on the electronic board.

Technical Specifications-
•	Mass: 1.4kg
•	Length: 166mm
•	Width: 220mm
•	Height: 49mm
•	operating temperature: -35 to 60 deg C
•	Pyrotechnical chain with a M5 interface
•	Radiation: 40 krad
•	Voltage: 12V or 28V DC
•	Differential SPI

Applications-
•	Solid rocket motors

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