The AMT Pegasus HP Turbo Jet Engine offers a thrust rating of 167N at standard temperature and pressure (S.T.P).
The engine casing diameter for the Pegasus HP is 120 mm.
The Pegasus HP can use various fuel types including Kerosene, Paraffin, Jet A1, JP4, and JP8.
The maximum allowed RPM for the Pegasus HP Turbo Jet Engine is 118,000.
The weight of the Pegasus HP Turbo Jet Engine with an airstart system is 2125 g, and with an electric start system, it weighs 2255 g.
The normal exhaust gas temperature for the Pegasus HP Turbo Jet Engine is 650°C.
The fuel consumption rate for the Pegasus HP Turbo Jet Engine is 500 g/min.
Yes, the Pegasus HP Turbo Jet Engine is designed for use in RC planes and other model aircraft.
The pressure ratio at maximum RPM for the Pegasus HP Turbo Jet Engine is 3.0.
Suitable oils for the Pegasus HP Turbo Jet Engine include AeroShell 500 and Mobil Jet oil II.
The engine length for the electric start engine version is 342 mm, and it weighs 2255 g.
The thrust at idle RPM for the Pegasus HP Turbo Jet Engine is 6 N.
The system airborne weight for the air start system with an additional high flow air solenoid valve is 2705 g.
The maximum exhaust gas temperature for the Pegasus HP Turbo Jet Engine is 750°C.
Yes, the Pegasus HP Turbo Jet Engine can be used in various drone applications, provided it's compatible with the system requirements.
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