Data for some military turbofan engines

 

Model no.

Thrust

(lb)*

TSFC (lb/hr) /lbf

Airflow (lb/sec)

OPR

D

(in)

L

(in)

Weight

(lb)

TIT

(F)

 

FPR

 

BR

 

Remarks

Fl00-PW-229

29,000
17,800

2.05
0.74

248

32.0

46.5

191

3,780

2,700

3.8

0.36

F-15, F16

Fl01-GE-102

30,780
17,390

2.460
0.562

356

26.8

55.2

180.7

4,448

2,550

2.31

1.91

B-lB

F103-GE-101

51,711

0.399

1,476

30.2

86.4

173

8,731

2,490

4.31

KC-10A

F107-WR-10l

635

0.685

13.6

13.8

12

48.5

141

2.1

1.0

Air Launch Cruise Missile

F108-CF-100

21,634

0.363

785

23.7

72

115.4

4,610

2,228

1.5

6.0

KC-135R

Fl10-GE-l00

28,000
18,330

2.08
1.47

254

30.4

46.5

182

3,895

2.98

0.80

F-16

Fl10-GE-l29

28,740
17,160

1.90
0.68

270

30.7

46.5

182

3,940

3.25

0.76

F-16

F117-PW-100

40,440

0.347

1264

31.8

84.5

146.8

7,100

1.71

5.44

(PW2040) C-17A

F118-GE-100

19,000

0.67

285

32.2

46.5

100.5

3,200

3.41

0.81

B-2

F119-PW-100

35,000

2.17

48

199

5,500

F-22 Raptor

F135-PW-400

43,000

28,000

308

28

51

220

3750

0.57

F-35 JSF

F138-GE-100

40,000

C-5M

F404-GE-F1D2

10,540

0.79

145.3

25

35

87

1,730

4.1

F-117A

F404-GE-400

16,000

1.85

26

35

154

2,195

0.34

F/A-18A/B, F-5G

F414-GE-400

22,000

13,000

170

30

35

154

2,445

F/A-18E/F

JT3D-3B

18,000

0.535

458

13.6

53

136.4

4,300

1,600

1.74

1.37

(TF33-102) EC/RC-l35

JT8D-7B

14,500

0.585

318

16.9

45

123.7

3.252

1,076

1.03

C-22, C-9, T-43A

TF30-P-111

25,100
14,560

2.450
0.686

260

21.8

49

241.7

3,999

2,055

2.43

0.73

F-111F

TF33-P-3

17,000

0.52

450

13.0

53

136

3,900

1,600

1.7

1.55

B-52H

TF33-P-7

21,000

0.56

498

16.0

54

142

4,650

1,750

1.9

1.21

C-141

TF34-GE-100

9,065

0.37

333

20.0

50

100

1,421

2,234

1.5

6.42

A-10

TF39-GE-1

40,805

0.315

1,549

26.0

100

203

7,186

2,350

1.56

8.0

C-5A

TF41-A-1B

14,500

0.647

260

20.0

40

114.5

3,511

2,165

2.45

0.76

A-7D, K

TFE731-2

3,500

0.504

113

17.7

40

50

625

1.54

2.67

C-21A

OPR = overall pressure ratio, FPR = fan pressure ratio, TSFC = thrust specific fuel consumption, TIT = turbine inlet temperature, BR = bypass ratio

*Maximum/Military Power @ SLS

Sources: The Engine Handbook, Directorate of Propulsion, Headquarters Air Force Logistics Command, Wright-Patterson AFB, Ohio, 1991-2011 and manufacturers’ literature