EvoJet evoJet-VX Series - Technical Specifications

evoJet B90 – B130vx – B160vx – Instructions 4.0
Technical Specifications
evoJet B90 – B130vx – B160vx
Max. thrust: B90: typ. 9 kg = 19 lb
B130: typ. 14 kg = 31 lb
B160: typ. 16 kg = 36 lb
Diameter: B90: 91 mm = 3.6 inches
B130/160: 112 mm = 4.4 inches
Length incl. starter: B90: 230 mm = 9.06 inches
B130/160: 288 mm = 11.3 inches
Weight: B90: 950 g = 2.1 lb
B130: 1595 g = 3.52 lb
B160: 1620 g = 3.58 lb
Rotor speed: B90: 45.000 – 165.000 rpm
B130: 30.000 – 119.000 rpm
B160: 30.000 – 123.000 rpm
Compressor: Alloy 2618 compressor 12-blade
Turbine: Axial-wheel Inconel
Fuel consumption: B90: max. 285 g = 10.0 oz./min.
B130: max. 420 g = 14.8 oz./min.
B160: max. 520 g = 18.4 oz./min.
Fuel type: Jet A1 / kerosene, approved fuel
with 5 % oil
Maintenance interval: B90: 300.000.000
B130/160: 200.000.000
corresponding 50 hours, see 24:JET-ENGINE
(page 19)
Status: October - 2010
(*) The engine thrust is electronically adjustable by setting the idle- and the full
thrust revolution speed (page 21, 30:ENGINE-IDLE und 31:ENGINE-100% ). All
performance data are related to International Standard Atmosphere, ISA and
optimal operating conditions which means, fuel, thrust tube and sufficient air
supply.
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