Turbojet engine 135KG thrust HX-1350N

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Turbojet engine 135KG thrust HX-1350N

Technical indicators

ITEM

Technical indicators

ITEM

Technical indicators

Maximum thrust

135daN

Maximum continuous thrust

120daN

Maximum speed

46000r/min

Fuel consumption rate

4.6L/min

Maximum length

750mm

 

 

Maximum outside diameter

265mm

Nozzle diameter

130mm

N.W

24kg

G.W

27kg

Exhaust temperature

≤800℃

Idling

25000r/min

Ground start time

≤120s

Push weight ratio

5

service life

≤24h

Storage life

5yearsq

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