下述信息為子型號400,子型號702動力輸出1000lbf
該機型為美國軍用
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:中國陜西聯合動力通用航空技術有限公司
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