Our in-house developed propulsion unit, called MR or “Motore a Razzo”, is powered by Liquid Oxygen and Kerosene.
EOS employs MR-2 engines, generating 25 kN of thrust.
During the reentry phase, a skip trajectory is employed to maximize the reentry time while reducing both thermal and mechanical loads.
Once lower down in the atmosphere, a parafoil is ejected, allowing a highly precise pinpoint landing.
Payload User Guide