ALTITUD

04/06/2014 GasTurb 11

-2.5 0 2.5 5 7.5 10 12.5 15 17.5*10 3Altitude [m]

32.6

32.7

32.8

32.9

33

33.1

33.2

Sp. Fuel C

onsumption [g/(kN

*s)]

Altitude = 500 ... 15000 [m]

1%

04/06/2014 GasTurb 11

-2.5 0 2.5 5 7.5 10 12.5 15 17.5*10 3Altitude [m]

540

560

580

600

620

640

660

680

700

Specific Thrust [m

/s]

Altitude = 500 ... 15000 [m]

04/06/2014 GasTurb 11

-2.5 0 2.5 5 7.5 10 12.5 15 17.5*10 3Altitude [m]

584

588

592

596

600

604

608

Nozzel E

xit Velocity V

8 [m/s]

Altitude = 500 ... 15000 [m]

04/06/2014 GasTurb 11

-2.5 0 2.5 5 7.5 10 12.5 15 17.5*10 3Altitude [m]

.46

.48

.5

.52

.54

.56

.58

Propulsive E

fficiency

Altitude = 500 ... 15000 [m]

MACH NUMBER

04/06/2014 GasTurb 11

0 .4 .8 1.2 1.6 2 2.4 2.8 3.2Mach Number

.1

.2

.3

.4

.5

.6

.7

.8

.9

1

Propulsive E

fficiency

Mach Number = 0,4 ... 2,72

04/06/2014 GasTurb 11

0 .4 .8 1.2 1.6 2 2.4 2.8 3.2Mach Number

0

40

80

120

160

200

240

280

320

Sp. Fuel C

onsumption [g/(kN

*s)]

Mach Number = 0,4 ... 5,04

1%

04/06/2014 GasTurb 11

0 .4 .8 1.2 1.6 2 2.4 2.8 3.2Mach Number

-200

0

200

400

600

800

1000

Specific Thrust [m

/s]

Mach Number = 0,4 ... 5,04

04/06/2014 GasTurb 11

0 .4 .8 1.2 1.6 2 2.4 2.8 3.2Mach Number

500

520

540

560

580

600

620

Nozzel E

xit Velocity V

8 [m/s]

Mach Number = 0,4 ... 5,04