Engine Progression
|
General Electric F110 Engine Family |
||||||||||
|
Engine Type |
Year |
Diameter |
Length |
Volume |
Thrust |
Thrust |
SFC |
Dry Weight |
Thrust per M3 |
Thrust Per Kg |
|
F110-GE-100 |
1984 |
46.5� |
182.3� |
0.436 |
-- |
28,000 lbf |
2.06 (Max) |
3,920 lbs |
29,128 kgf/m3 |
7.14 kgf/kg |
|
F110-GE-129 |
1992 |
46.5� |
182.3� |
0.436 |
-- |
29,000 lbf |
1.9 (Max) |
3,980 lbs |
30,170 kgf/m3 |
7.29 kgf/kg |
|
F110-GE-132 |
2003 |
46.5� |
181.9� |
0.435 |
-- |
32,000 lbf |
2.09 (Max) |
4,050 lbs |
33,368 kgf/m3 |
7.9 kgf/kg |
|
General Electric F404 Engine Family |
||||||||||
|
Engine Type |
Year |
Diameter |
Length |
Volume |
Thrust |
Thrust |
SFC |
Dry Weight |
Thrust per M3 |
Thrust Per Kg |
|
F404-GE-400 |
-- |
35� |
154� |
0.277 |
-- |
16,000 lbf |
1.85 |
2,195 lbs |
26,199 kgf/m3 |
7.29 kgf/kg |
|
F404-GE-402 |
-- |
35� |
154� |
0.277 |
-- |
17,700 lbf |
1.74 |
2,282 lbs |
28,986 kgf/m3 |
7.76 kgf/kg |
|
F414-GE-400 |
1998 |
35� |
154� |
0.277 |
-- |
22,000 lbf |
|
2,444~ lbs |
36,025 kgf/m3 |
9 kgf/kg |
|
Pratt and Whitney J79 Engine Family |
||||||||||
|
Engine Type |
Year |
Diameter |
Length |
Volume |
Thrust |
Thrust |
SFC |
Dry Weight |
Thrust per M3 |
Thrust Per 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 |
Thrust |
Thrust |
SFC |
Dry Weight |
Thrust per M3 |
Thrust Per 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 |
Thrust |
Thrust |
SFC |
Dry Weight |
Thrust per M3 |
Thrust Per 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 |
||
|
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 |
|
Late 1945 |
5,200 lbf |
1,840 lbf |
|
Engine Power List |
|||||||||
|
Actual Power Plants |
|||||||||
|
Engine Type |
Specific Power |
Power/Volume Ratio |
Specific Fuel Consumption |
||||||
|
Wright R-3350 Duplex Cyclone Radial |
0.739 |
381.085 |
|
||||||
|
Allison V-1710 V-12 |
0.572 |
727.632 |
|
||||||
|
Pratt & Whitney R-2800-54 Double Wasp Radial |
|
|
|
||||||
|
Pratt & Whitney R-4360 CB2 Wasp Major
Radial |
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 |
1.54 |
689 |
231 |
||||||
|
Barnaulttransmash UTD-20 V-6 Diesel |
3.032 |
303.014 |
143 |
||||||
|
Barnaulttransmash UTD-29 V-10 Diesel |
2.440 |
509.465 |
136.57 |
||||||
|
Barnaulttransmash KD-34 V-12 Diesel |
1.367 |
595.507 |
113.28 (average) |
||||||
|
PZL-WOLA Model S12-U V-12 Diesel |
1.568 |
522.521 |
Unknown |
||||||
|
PZL-WOLA Model W55-U V-12 Diesel |
2.039 |
358.186 |
Unknown |
||||||
|
PZL-WOLA Model W-6B.AX Inline-6 Diesel |
4.830 |
142.867 |
Unknown |
||||||
|
MTU MB 873 Ka-501 V-12 Diesel |
2.355 |
298.597 |
Unknown |
||||||
|
MTU MB 871 Ka-501 V-8 Diesel |
1.932 |
430.942 |
Unknown |
||||||
|
MTU MT 883 Ka 523 V-12 Diesel |
1.354 |
554.915 |
Unknown |
||||||
|
MTU MB 833 Aa-501 V-6 Diesel |
3.182 |
260.132 |
Unknown |
||||||
|
MTU MB 833 Ka-501 V-6 Diesel |
2.272 |
492.673 |
Unknown |
||||||
|
MTU MB 837 Ka-501 V-8 Diesel |
1.980 |
492.385 |
Unknown |
||||||
|
MTU MB 838 Ka-501 V-10 Diesel |
1.796 |
369.202 |
Unknown |
||||||
|
MTU MT 883 Ka 500 V-12 Diesel |
1.591 |
1042.586 |
Unknown |
||||||
|
MTU MT 881 V-8 Diesel |
1.688 |
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|
Unknown |
||||||
|
NORINCO 12150L V-12 Diesel |
2.308 |
302.082 |
144.61 |
||||||
|
NORINCO 12150L-7BW V-12 Diesel |
1.603 |
450.850 |
140.59 |
||||||
|
NORINCO X150-960 V-12 Diesel |
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% |