1) Performance Graphs For Stand. Conditions (Isa)10 - Rotax 912 series Operator's Manual

10.1.2.1) Performance graphs for stand. conditions (ISA)
130
120
110
100
90
80
70
60
50
40
30
20
10
0
2500 3000
fig. 12
30
25
20
Werte bezogen auf die
15
Propeller-Kurve
values along propeller
10
5
0
2500 3000
fig. 13
Effectivity: 912 ULS / S
OM initial issue
Drehmoment
Torque
max. Motorleistung
max. engine output
3500 4000
Drehzahl / Engine Speed [1/min]
Ansaugladedruck
manifold pressure
curve
3500 4000
Drehzahl/Engine speed [1/min / rpm]
AIRCRAFT ENGINES
Propellerkurve
power requirement of
propeller
4500 5000
Benzinverbrauch
fuel consumption
4500 5000
130
125
120
115
110
105
100
95
90
5800
5500
02001
30
25
20
15
10
5
0
5800
5500
02002
page 10 - 7
July 01/98