[1][2] The engine is a four stroke, 90° V twin cylinder, four valve, 1,225 cc (75 cu in) powerplant that delivers a maximum of 115 hp (86 kW) at 7000 rpm and is capable of inverted flight as well as tractor and pusher configuration installations.

It is equipped with a 2.95-to-1 reduction gearbox and has a dry weight of 67 kg (147 lbs).

It incorporates an automatic decompressor starter installed on the exhaust valve camshaft.

[1][2] The family of engines is expected to produce 80 to 150 hp (60 to 112 kW) when fully developed, although the initial version is expected to produce 115 hp (86 kW).

On initial runs it produced 135 hp (101 kW)[1] The first flight on an ICP Savannah S test bed aircraft was on 18 December 2014.