The B150 was designed to comply with the French CNSK rules. It features a single main rotor and tail rotor, a two-seats-in side-by-side configuration enclosed cockpit with a bubble windshield, skid landing gear and a 1600NaN0 Solar T62T-32 turboshaft engine.[1]
The aircraft fuselage is made from aluminum and composites. Its two-bladed rotor has a diameter of 7.671NaN1 and a chord of 191NaN1. The aircraft has a typical empty weight of 4000NaN0 and a gross weight of 7000NaN0, giving a useful load of 3000NaN0. With full fuel of the payload for the pilot, passenger and baggage is 1570NaN0.[1]
Reviewer Werner Pfaendler, describes the design as providing "easy and fun flying".[1]
Production of the B150 was suspended due to deficiencies in the Solar T62 powerplant. The company said, "it was decided to abandon the Solar T62 turbine; this second-hand power source appeared to be obsolete, difficult to find in a proper condition and with limited performance". Instead the company redesigned the airframe to accept a 2000NaN0 piston engine as the B200 and also a 2500NaN0 TS100 turboshaft engine as the B250.[2]