|
|
 |
 |
Mono-cylinder engine suitable for one-seat hang-gliders, motor-gliders and two seats paramotors |
| SCHEDULE
OF STATIC THRUST |
Engine MINI 3
matriculation M3002
Poly-V belt reduction, ratio 1:245
Double blades pushing propeller
wood made
152 x 108 GT |
| TESTING
CONDITIONS |
T 1°C -
P 1057 Mb - UR 45%
Locality Torre Maina 04/01/2002
Altitude (S.L.M.) 300 m |
| RPM |
Consumption
l/hr |
Kg
of thrust |
| 6800 |
5,8 |
102 |
| 6600 |
5,6 |
97 |
| 6400 |
5 |
94 |
| 6000 |
4 |
86 |
| 5500 |
3 |
78 |
| 5000 |
2,8 |
73 |
| 4500 |
2,4 |
61 |
| 4000 |
2 |
54 |
|
|
|
TECHNICAL DATA
|
|
Displacement
|
cc
|
270
|
|
Bore
|
mm
|
72.8
|
|
Stroke
|
mm
|
65
|
| Compression Ratio |
10,1/1
|
|
Power
|
Hp
|
36
|
|
kW
|
23,7
|
|
RPM
|
7.000
|
| Weight of the
engine ready to fly |
Kg 22
|
| Lamellar intake with Bing 36
mm carburetor |
| Alluminium cylinder with Nikasil
ceramic coating |
| Air-cooling |
| Exhaust resonance system. Poly-V
belt reduction |
| Electronic ignition with alternator
to recharge battery in fly |
| Electric starter |
| Premix two stroke oil in gasoline,
2,5% oil by volume to leaded fuel, 3% oil by volume to
unleaded fuel |
|
REDUCTION RATIO AVAIABLE
|
|
1:249 - 1:257 - 1:276
|
|
|
| POWER
AND TORQUE |
 |
| RPM |
Hp |
kW |
Kgm |
| 4000 |
12,8 |
9,42 |
2,29 |
| 4500 |
15,3 |
11,26 |
2,43 |
| 5000 |
16 |
11,78 |
2,43 |
| 5500 |
24 |
17,66 |
2,72 |
| 6000 |
27,4 |
20,17 |
3,29 |
| 6500 |
29,9 |
22,01 |
4,08 |
| 7000 |
32,2 |
23,7 |
3,29 |
| 7500 |
30 |
22,08 |
2,86 |
| |
|
|
