The separation system is intended to fasten a microsatellite to the launch vehicle, to separate it and then to move it away
The separation system is intended to fasten a microsatellite (≤ 100 kg) to the launch vehicle, to separate it and then to move it away (Vz ≈ 1 to 3 m/s).
The separation system uses an hermetic expansible tube, four to ten springs move the satellite away.
Initiation is realized through two 1DPWH30 type detonators.
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