Engine Progression

General Electric F110 Engine Family

Engine Type

Year

Diameter

Length

Volume
(m3)

Thrust
(Dry)

Thrust
(After)

SFC

Dry Weight

Thrust per M3
(kgf/m3)

Thrust Per Kg
(kgf/kg)

F110-GE-100

1984
(0 Years)

46.5”

182.3”

0.436

--

28,000 lbf
(12,700 kgf)

2.06 (Max)

3,920 lbs
(1,778 kg)

29,128 kgf/m3

7.14 kgf/kg

F110-GE-129

1992
(8 Years)

46.5”

182.3”

0.436

--

29,000 lbf
(13,154 kgf)

1.9 (Max)

3,980 lbs
(1,805 kg)

30,170 kgf/m3

7.29 kgf/kg

F110-GE-132

2003
(19 Years)

46.5”

181.9”

0.435

--

32,000 lbf
(14,515 kgf)

2.09 (Max)

4,050 lbs
(1,837 kg)

33,368 kgf/m3

7.9 kgf/kg


General Electric F404 Engine Family

Engine Type

Year

Diameter

Length

Volume
(m3)

Thrust
(Dry)

Thrust
(After)

SFC

Dry Weight

Thrust per M3
(kgf/m3)

Thrust Per Kg
(kgf/kg)

F404-GE-400

--

35”

154”

0.277

--

16,000 lbf
(7,257 kgf)

1.85

2,195 lbs
(996 kg)

26,199 kgf/m3

7.29 kgf/kg

F404-GE-402

--

35”

154”

0.277

--

17,700 lbf
(8,029 kgf)

1.74

2,282 lbs
(1,035 kg)

28,986 kgf/m3

7.76 kgf/kg

F414-GE-400

1998

35”

154”

0.277

--

22,000 lbf
(9,979 kgf)


2,444~ lbs
(1,109~ kg)

36,025 kgf/m3

9 kgf/kg


Pratt and Whitney J79 Engine Family

Engine Type

Year

Diameter

Length

Volume
(m3)

Thrust
(Dry)

Thrust
(After)

SFC

Dry Weight

Thrust per M3
(kgf/m3)

Thrust Per Kg
(kgf/kg)

J79-GE-2






15,000 lbf





J79-GE-5A






15,600 lbf





J79-GE-7A






15,800 lbf





J79-GE-8


38.3"

208.5"



17,000 lbf

1.93 (max)

3,695 lbs



J79-GE-10


39.1"

208.7"



17,860 lbf





J79-GE-15


38.3"

208.4"



17,000 lbf

1.94 (max)

3,699 lbs



J79-GE-17


39.1"

208.7"



17,900 lbf





J79-GE-119












General Electric/Allison J33 Engine Family

Engine Type

Year

Diameter

Length

Volume
(m3)

Thrust
(Dry)

Thrust
(After)

SFC

Dry Weight

Thrust per M3
(kgf/m3)

Thrust Per Kg
(kgf/kg)

J33-GE-11

1944




3,850 lbf

N/A





J33-A-17

1946




4,000 lbf

N/A





J33-A-21

1947




4,500 lbf

N/A





J33-A-23

1948




4,600 lbf

N/A





J33-A-35

1949




4,600 lbf

5,400 lbf (water inject)






R-11 Engine Family

Engine Type

Year

Diameter

Length

Volume
(m3)

Thrust
(Dry)

Thrust
(After)

SFC

Dry Weight

Thrust per M3
(kgf/m3)

Thrust Per Kg
(kgf/kg)

R-11F-300






6,120 kgf





R-11F2-300






6,120 kgf





R-11F2S-300






6,175 kgf






General Electric LM Family of Marine Gas Turbines

Engine Type

Year

Length (m)

Height (m)

Volume (M3)

Weight (lb)

Output (shp)

SFC (lb/shp/hr)

Exhaust Gas Flow (Lb/sec)

HP per M3

HP per kg

LM500

1981

2.96

0.91

2.69 m3

1,990

6,000

0.443

35.9

2,228

--

LM1600

1988

4.24

2.03

8.61 m3

8,200

20,000

0.376

104

2,324

--

LM2500

1969

6.52

2.04

13.3 m3

10,300

33,600

0.373

155

2,526

--

LM2500+

1998

6.7

2.04

13.67 m3

11,545

40,500

0.354

189

2,963

--

LM6000

1991

7.3

2.5

18.25 m3

18,010

57,300

0.329

273

3,140

--


Best Jet Engine Thrusts of WWII
(Courtesy of Stuart Slade)

Date

Anglo-American

German

Mid 1943

1,400 lbf

1,600 lbf

Early 1944

1,700 lbf

1,600 lbf

Mid 1944

2,000 lbf

1,800 lbf

Late 1944

3,400 lbf

1,840 lbf

Early 1945

4,000 lbf

1,840 lbf

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5,200 lbf

1,840 lbf


Engine Power List

Actual Power Plants

Engine Type
Craft used in

Specific Power
(kg/kw)

Power/Volume Ratio
(kW/m3)

Specific Fuel Consumption
(grams per kWh)

Wright R-3350 Duplex Cyclone Radial
B-29

0.739

381.085


Allison V-1710 V-12
Aircraft blah

0.572

727.632


Pratt & Whitney R-2800-54 Double Wasp Radial




Pratt & Whitney R-4360 CB2 Wasp Major Radial
B-50, B-36, C-97, C-119, C-124

0.638

485.258

156.66

Ukrainian GTD-1250 Gas Turbine (T-80)

1.13

674.28

300

American AGT-1500 Gas Turbine

1.013

797.194


SACM V8X-1500 Hyperbar V-8 Diesel
LeClerc

1.54

689

231

Barnaulttransmash UTD-20 V-6 Diesel
BMP-1 and BMP-2

3.032

303.014

143

Barnaulttransmash UTD-29 V-10 Diesel
BMP-3

2.440

509.465

136.57

Barnaulttransmash KD-34 V-12 Diesel
T-72

1.367

595.507

113.28 (average)
(85.96 to 140.59 range)

PZL-WOLA Model S12-U V-12 Diesel
T-72

1.568

522.521

Unknown

PZL-WOLA Model W55-U V-12 Diesel
T-55 and T-62s

2.039

358.186

Unknown

PZL-WOLA Model W-6B.AX Inline-6 Diesel
PT-76

4.830

142.867

Unknown

MTU MB 873 Ka-501 V-12 Diesel
Leopard 2

2.355

298.597

Unknown

MTU MB 871 Ka-501 V-8 Diesel
Type 88 (K-1) MBT

1.932

430.942

Unknown

MTU MT 883 Ka 523 V-12 Diesel
Power Demonstration Unit

1.354

554.915

Unknown

MTU MB 833 Aa-501 V-6 Diesel
M41, M44, M52 Repowering

3.182

260.132

Unknown

MTU MB 833 Ka-501 V-6 Diesel
AMX-30 Repowering

2.272

492.673

Unknown

MTU MB 837 Ka-501 V-8 Diesel
Chieftain Repowering

1.980

492.385

Unknown

MTU MB 838 Ka-501 V-10 Diesel
Arjun MBT

1.796

369.202

Unknown

MTU MT 883 Ka 500 V-12 Diesel
Euro Power Pack for LeLerc Tropic

1.591

1042.586

Unknown

MTU MT 881 V-8 Diesel
PzH 2000 Engine

1.688

1027.076

Unknown

NORINCO 12150L V-12 Diesel
Type 59 MBT Engine

2.308

302.082

144.61

NORINCO 12150L-7BW V-12 Diesel
Type 69 MBT Engine

1.603

450.850

140.59

NORINCO X150-960 V-12 Diesel
Possibly Type 85-III MBT Engine

2.235

575.069

140.59

Idealized Power Plants

Engine Type

Specific Power (kg/kw)

Power/Volume Ratio

(kW/m3)

Specific Fuel Consumption

(grams per kWh)

GURPS Late TL05 (1850s-1900s) Gasoline Engine

9.69

82.67

191.33

GURPS TL05 (1700-1900) Early Steam

48.44

16.53

286.99

GURPS TL05 (1700-1900) Forced Draft Steam

36.33

22.04

255.1

GURPS TL05 (1700-1900) Triple Expansion Steam

24.22

33.07

223.21

GURPS TL06 (1900-1950) Diesel Engine

5.62

142.4

127.55

GURPS TL06 (1900-1950) Gasoline Engine

2.86

280.28

159.44

GURPS TL06 (1900-1950) Steam Turbine

14.42

55.53

190.51

GURPS TL07 (1951-2000) Fission Plant

126.97

6.31

0

GURPS TL07 (1951-2000) Steam Turbine

11.54

69.41

159.44

GURPS TL09 (2050 and beyond) Fusion Plant

91.17

8.78

0

GURPS TL11 (Interstellar) Antimatter Plant

18.19

44.03

0

Modern Nuclear RTGs (Galileo Space Probe)

185

19.94

0

Nuclear Gas Turbine (Shielding and fuel included)

41.94

3.73

0

Nuclear PWR Plant (Fuel plus Shielding)

151

3.73

0

PEM Fuel Cell (1997)

2.81

212.77

200



Growth Potential of Mature Technologies, such as modern afterburning turbofans

Year

Percentage Growth over Base Model in kgf/m3

Percentage Growth over Base model in kgf/kg

0

BASE MODEL

BASE MODEL

1

0.24%

0.07%

2

0.55%

0.20%

3

0.91%

0.38%

4

1.32%

0.62%

5

1.80%

0.91%

6

2.33%

1.25%

7

2.93%

1.65%

8

3.58%

2.10%

9

4.29%

2.61%

10

5.05%

3.17%

11

5.88%

3.78%

12

6.76%

4.45%

13

7.70%

5.17%

14

8.70%

5.95%

15

9.75%

6.78%

16

10.87%

7.66%

17

12.04%

8.60%

18

13.27%

9.60%

19

14.56%

10.64%

20

15.90%

11.75%

21

17.31%

12.90%

22

18.77%

14.11%

23

20.29%

15.37%

24

21.87%

16.69%

25

23.50%

18.06%

26

25.20%

19.49%

27

26.95%

20.97%

28

28.76%

22.50%

29

30.63%

24.09%

30

32.55%

25.74%



Growth Potential of Immature Technologies, such as Turbojet engines in the 1940s

Months

Percentage Growth over Base Model in thrust

0

BASE MODEL

1

5.11%

2

10.48%

3

16.13%

4

22.06%

5

28.30%

6 (0.5 Years)

34.85%

7

41.75%

8

48.99%

9

56.60%

10

64.60%

11

73.02%

12 (1 Year)

81.86%

13

91.15%

14

100.92%

15

111.18%

16

121.98%

17

133.32%

18 (1.5 Years)

145.24%

19

157.77%

20

170.95%

21

184.79%

22

199.34%

23

214.64%

24 (2 Years)

230.72%

25

247.62%

26

265.38%

27

284.05%

28

303.68%

29

324.31%

30 (2.5 Years)

345.99%

31

368.78%

32

392.73%

33

417.91%

34

444.38%

35

472.20%

36 (3 Years)

501.44%