Page 151 - Aeronautical Engineer Data Book
P. 151
35 000 36 089 35 000 35 000 35 000 35 000 35 000 35 000 35 000 35 000 0.75 0.85 0.8 0.82 0.83 0.8 0.8 0.8 0.8 0.8 3307 11813 2550 11500 5725 518
35 000 0.83 0.545 5.181 3.404 16 644 2 1+3LP 10HP 2HP 6LP
0.562 4.343 2.794 10 726 2 1+4LP 14HP 2HP 5LP
2.616 1.245 1670 2 1F +14cHP 2HP 4LP
35 000 0.8 0.545 2.616 1.945 5700 2 1+4LP 9HP 1HP 5LP
40 000 0.8 1310 0.645 2.514 1.219 1325 2 1+5LP +1CF 2HP 3LP
0.414 1.62 1.272 1385 2 various 2HP 2LP
Cruise Altitude (ft) Mach number Thrust (lb) Thrust lapse rate Flat rating (°C) SFC (lb/hr/lb) Dimensions Length (m) Fan diameter (m) Basic eng. weight (lb) Layout Numbe
