100 - 300hp piston engine JPE 02 H Hybrid

100 - 300kgfor light aircraft4-stroke

Fuel - Diesel fuel Engine type - 4 in line – turbo diesel common rail engine Bore mm - 75 Stroke mm - 88.3 Cubic capacity - 1540 cc Peak chamber pressure - 180 bar Idle speed - rpm 1000 Max. engine speed - rpm 4000 Dimensions Overall length - mm 776 Overall width - mm 571 Overall height - mm 592 Other Informations Timing system - Single level FADEC with Engine parameters Monitorcapability, UAV1553B Bus communication system,capability for compliances with DO178-B Oil lubrication andcooling - 1 mechanically gearedmaximum pressure allowed 6 bar.Maximum allowable oil consumption 1kg every 25h.Maximum allowable temperature 160°C Oil type and quantity - SAE 5W30 synthetic oil API SL/CF ACEA A3/B3/B4Mercedes Benz 229.3, 4.5 kg Oil filter - Internal cartridge type PRSU (Prop. Red. Speed Unit) - 1.6:1 ratio, Electric Pitch actuator Temperature range - +/- 55°C ISA Fuel injection - Fully electronic, 1 injectors per cylinder. DC supply with onboard aircraft battery and aircraft DC generator. Engine mounts - Rubber shock mounts required. Service angles - Bank: 20°.Pitch: +25°/-25° G loads - According to FAA 1.1 and 23.3 aerobatic categoryInverted flight allowed only with special kit TBO - 2,000h for standard use.