Products > G-360-TS

Turbocharged 360 hp 3-rotor gasoline engine, for experimental market, complete with Digital Engine Management system. Runs on avgas 100LL as well as mogas 87 octane or higher. Prototype was presented at Air Venture 2006 in Oshkosh.

SpecificationS G-360-TS (projected)

 

Engine Type Turbocharged rotary
Number of Rotors 3
Displacement 3x654cc (3x39.9 cu.in.) per rotor
Cooling Coolant: water / ethylene glycol
Coolant heat load: 90kW / 309kBTU/hr
Oil heat load: 44kW / 150kBTU/hr
Intercooler load: 22kW / 76kBTU/hr
Engine Management Fully redundant dual-ECU digital control
Fuel System Dual electronic injection
Dual electric fuel pumps
Recommended Fuel 100LL avgas
Leaded or unleaded mogas (US: 90, Europe: 95)
PSRU 6-pinion planetary, ratio 2.8235:1
Hydraulic CS propeller governor drive
Propeller Rotation Tractor configuration: clockwise
Pusher configuration: anti-clockwise
Max. Take-off power 360 hp @ 2,250 propeller rpm (5 mn limit)
Max. Continuous Power 320 hp @ 2,150 propeller rpm
75% Cruise Power 270 hp @ 2,000 propeller rpm or below
Weight¹ 190kgs / 420 lbs
Daul Alternators 14V 70 Amp or 28V 40A

¹ Dry engine, PSRU weight including starter, main alternator included

Fact Sheet:

Fiche_G360-TS.pdf 1.18 MB