下述信息为子型号400，子型号702动力输出1000lbf

该机型为美国军用

General characteristics

Type: Turbojet

Length: 29 in (74 cm)

Diameter: 12.5 in (32 cm)

Dry weight: 101.5 lb (46 kg)

Components

Compressor: Single stage axial compressor, single stage centrifugal compressor

Combustors: Annular

Turbine: Single stage high pressure turbine

Performance

Maximum thrust: 660 lbf (2.9 kN)

Overall pressure ratio: 5.6:1

Specific fuel consumption: 1.2 lb/(lbf⋅h) or 34 g/(kN⋅s)

Thrust-to-weight ratio: 6.5

提供商：中国陕西联合动力通用航空技术有限公司