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airplane
Created by MET@SPACE
...498ia engine
498ia engine
Engine
498ia
Type
opposed two cylinder two stroke boxer
Output
39Hp at 6700 rev/min
Total displacement
498 cm3
Cooling system
air > 25 m/sec
Max rpm
7000 rev/min
Min rpm
1800 to 2200 rev/min
Bore
75 mm
Stroke
56mm
Bore/stroke ratio
1,339
Compression ratio
10.6:1
Cylinders
light alloy metal ceramic plated castings
Cylinder heads
light alloy castings
Crankcase
machined from solid
Connecting rods
forged steel with caged needle bearings at both ends
Crankshaft
forget steel supported by special double-row ball bearings
Fuel metering
fuel injection on throttle body
Ignition system
programmed inductive discharging system managed by ECU
Spark plug
NGK C8HIX
Exhaust system
stub
TBO
250 hours
Communication from ECU to client system by
RS232
Operating temperature
-20 +55°C
Alternator
28V-60A
Operating temperatures
Temperature under spark plug (CHT)
max 260° C
Exhaust gas temperature (EGT)
max 580° C
Acceleration
Operating (engine working)
launch 15g along propeller axis
Operating (engine working)
operation 7g along vertical and 1g along side axis
Non operating (engine non-working)
+- 15g along all axes
Rotation
counter clockwise(when looking on propeller side
Fuel
>=95 Oct. petrol/oil mixture 2% synthetic oil for 2 stroke engines
Weight with alternator
18,6Kg
Weight/power ratio
0.476
Specific consumption
Better than 330gr./Hp/h
details details
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PDF
PDF
498ia