下述信息為子型號400，子型號702動力輸出1000lbf

該機(jī)型為美國軍用

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：中國陜西聯(lián)合動力通用航空技術(shù)有限公司