Sino-Engines HQ200WP

Name: Sino-Engines HQ200WP
Brand: Sino-Engines

The Sino-Engines HQ200WP is a compact, single-shaft turbojet engine for high-performance target aircraft and UAVs. It combines a single-stage centrifugal compressor, annular straight-through combustion chamber and single-stage turbine, with electrical supply capability of 2.5 kW at 28.0 V.

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Product overview

The Sino-Engines HQ200WP turbojet engine is intended for high-performance target aircraft and UAVs. Its compact single-shaft construction combines a single-stage centrifugal compressor, an annular straight-through combustion chamber and a single-stage turbine. The engine has an overall pressure ratio of 3.8 and a turbine inlet temperature of 1223 K (950 °C).

Takeoff specific fuel consumption is 1.12 kg/(kgf.h). The HQ200WP has a starting time of 55 seconds and a starting altitude range of 0–4500 m. Its electrical supply capability is 2.5 kW at 28.0 V.

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Specifications

Sino-Engines HQ200WP specifications
Specification	Value & conditions
Model	HQ200WP engine
Product type	Turbojet engine
Applications	High-performance target aircraft and UAVs
Construction	Compact single-shaft design with a single-stage centrifugal compressor, annular straight-through combustion chamber and single-stage turbine
Specific fuel consumption	1.12 kg/(kgf.h)Takeoff.
Overall pressure ratio	3.8
Turbine inlet temperature	1223 K (950 °C)
Starting time	55 s
Electrical supply capability	2.5 kW / 28.0 V
Starting altitude	0–4500 mEngine starting.