Aircraft;
engine; and references |
b | S | A | Wmax | Wg | We | T/Wg | Wg/S | ||
---|---|---|---|---|---|---|---|---|---|---|
Messerschmidt Me 262A; two Junkers Jumo turbojets of 1984 lb thrust each; |
41.1 |
34.8 |
233.6 |
7.23 |
c 18.5 |
15 720 |
14 101 |
8 378 |
0.28 |
60.4 |
Gloster Meteor F.Mk.4; two Rolls Royce Derwent 5 turbojets of 3500 lb thrust each; |
37.1 |
41.0 |
350.0 |
3.93 |
0 |
18 000 |
15 000 |
10 050 |
0.47 |
43.0 |
Bell P-59A; two General Electric J31-GE-5 turbojets of 2000 lb thrust each; |
45.5 |
38.9 |
385.0 |
5.38 |
0 |
13 000 |
10 822 |
7 950 |
0.37 |
28.1 |
Lockheed P-80A; one Allison J33-A-11 turbojet of 4000 lb thrust; |
38.9 |
34.5 |
237.6 |
6.37 |
0 |
14 000 |
11 700 |
7 920 |
0.34 |
49.2 |
McDonnell FH-1; Two Westinghouse J30-WE-20 turbojets of 1560 lb thrust each; |
40.8 |
38.8 |
274.0 |
6.08 |
0 |
12 500 |
9 974 |
6 699 |
0.31 |
36.4 |
North American F-86E; One General Electric J47-GE-13 turbojet of 5200 lb thrust; |
37.1 |
37.5 |
287.9 |
4.78 |
35.0 |
17 806 |
14 856 |
10 845 |
0.35 |
51.6 |
Grumman F9F-8; One Pratt & Whitney J48-P-8 turbojet of 7250 lb thrust; |
34.5 |
42.1 |
337.0 |
3.53 |
35.0 |
24 763 |
20 098 |
11 866 |
0.36 |
59.6 |
North American F-100D; One Pratt & Whitney J57-P-21 turbojet of 16000/10000 lb thrust; |
38.8 |
49.3 |
400.2 |
3.76 |
45.0 |
- |
34 050 |
20 638 |
0.47 |
85.1 |
Convair F-106A; One Pratt & Whitney J75-P-17 turbojet of 24000/16100 lb thrust; |
38.3 |
70.7 |
697.8 |
2.10 |
c 60.0 |
- |
34 510 |
24 038 |
0.70 |
49.5 |
Lockheed F-104G; one General Electric J79-GE-11A turbojet of 15600/10000 lb thrust; |
21.9 |
54.8 |
196.1 |
2.45 |
0 |
29 083 |
27 300 |
13 996 |
0.57 |
139.2 |
Republic F-105D; one Pratt & Whitney J75-P-19W turbojet of 24500/10000 lb thrust; |
34.9 |
64.3 |
385.0 |
3.16 |
45.0 |
52 838 |
48 976 |
26 855 |
0.50 |
127.2 |
Vought F-8H; one Pratt & Whitney J57-P-420 turbojet of 16000/12400 lb thrust; |
35.8 |
54.2 |
375.0 |
3.42 |
35.0 |
34 200 |
29 200 |
18 700 |
0.57 |
77.8 |
McDonnell F-4E; two General Electric J79-GE-17 turbojets of 17900/11110 lb thrust each; |
38.3 |
63.0 |
530.0 |
2.77 |
c 45.0 |
61 651 |
53 848 |
29 535 |
0.66 |
101.6 |
Northrop F-5E; Two General Electric J85-GE-21 turbojets of 5000/3500 lb thrust each; |
26.8 |
48.2 |
186.0 |
3.86 |
24.0 |
20 486 |
15 745 |
9 588 |
0.64 |
84.7 |
General Dynamics F-111D; Two Pratt & Whitney TF30-P-9 turbofans of 20840/12430 lb thrust each; |
b 63/32 |
73.5 |
525.0 |
b 7.56/1.95 |
b 16/72.5 |
98 850 |
82 819 |
46 172 |
0.50 |
157.8 |
Grumman F-14A; Two Pratt & Whitney TF30-P-412A turbofans of 20000/12500 lb thrust each; |
b 64.1/37.6 |
62.0 |
565.0 |
b 7.3/2.5 |
b 20/68 |
74 348 |
70 345 |
39 930 |
0.57 |
124.5 |
McDonnell Douglas F-15C; two Pratt & Whitney F100-PW-100 turbofans of 23904/14780 lb thrust each; |
42.8 |
63.8 |
608.0 |
3.01 |
c 45.0 |
68 000 |
44 500 |
28 700 |
1.07 |
73.2 |
General Dynamics F-16A; one Pratt & Whitney F100-PW-200 turbofans of 23830/14800 lb thrust each; |
35.0 |
47.6 |
300.0 |
4.08 |
c40.0 |
34 500 |
23 357 |
14 567 |
1.02 |
77.9 |
British Aerospace Harrier AV-8A; one Rolls-Royce Pegasus 103 turbofan of 21500 lb thrust; |
25.3 |
47.6 |
201.1 |
3.18 |
34.0 |
26 000 |
18 000 |
12 140 |
1.19 |
89.5 |
Aircraft;
engine; and references |
Vmax High Altitude |
Vmax Low Altitude |
Ve | hSL | T | hCE | Ferry range, miles | f | CD,0 | (L/D) max | First flight d |
---|---|---|---|---|---|---|---|---|---|---|---|
Messerschmidt Me 262A; two Junkers Jumo turbojets of 1984 lb thrust each; |
540 (M= 0.76) at h=19 685 |
514 (M=0.67) at h=0 |
- |
3 939 |
- |
- |
528 |
- |
- |
- |
3/25/42 |
Gloster Meteor F.Mk.4; two Rolls Royce Derwent 5 turbojets of 3500 lb thrust each; |
570 (M= 0.81) at h=20 000 |
585 (M= 0.77) at h=0 |
520 |
7 500 |
5.0 (h=30 000) |
- |
1 000 |
- |
- |
- |
3/5/43 |
Bell P-59A; two General Electric J31-GE-5 turbojets of 2000 lb thrust each; |
413 (M= 0.61) at h=30 000 |
380 (M= 0.51) at h=5 000 |
375 |
3 200 |
15.5 (h=30 000) |
46 200 |
375 |
- |
- |
- |
10/1/42 |
Lockheed P-80A; One Allison J33-A-11 turbojet of 4000 lb thrust; |
508 (M= 0.75) at h=30 000 |
558 (M= 0.73) at h=0 |
410 |
4 580 |
5.5 (h=20 000) |
45 000 |
540 |
3.2 |
0.0134 |
17.7 |
1/8/44 |
McDonnell FH-1; two Westinghouse J30-WE-20 turbojets of 1560 lb thrust each; |
485 (M= 0.67) at h=15 000 |
472 (M= 0.62) at h=0 |
307 |
4 000 |
11.0 (h=30 000) |
34 500 |
910 |
- |
- |
- |
1/26/45 |
North American F-86E; one General Electric J47-GE-13 turbojet of 5200 lb thrust; |
601 (M= 0.91) at h=35 000 |
679 (M= 0.89) at h=0 |
537 |
7 250 |
6.3 (h=30 000) |
47 200 |
1 022 |
3.8 |
0.0132 |
15.1 |
10/1/47 |
Grumman F9F-8; one Pratt & Whitney J48-P-8 turbojet of 7250 lb thrust; |
593 (M= 0.89) at h=35 000 |
647 (M= 0.86) at h=2 000 |
516 |
4 800 |
8.3 (h=30 000) |
42 000 |
1312 |
- |
- |
- |
9/20/51 |
North American F-100D; one Pratt & Whitney J57-P-21 turbojet of 16000/10000 lb thrust; |
927 (M= 1.39) at h=35 000 |
639 (M= 0.97) at h=0 |
587 |
22 400 |
- |
51 300 |
1971 |
5.0 |
0.0130 |
13.9 |
5/25/53 |
Convair F-106A; one Pratt & Whitney J75-P-17 turbojet of 24000/16100 lb thrust; |
1 525 (M= 2.31) at h=40 000 |
- |
- |
- |
6.9 (h=51 800) |
52 700 |
1809 |
5.8 |
0.0083 |
12.1 |
12/26/56 |
Lockheed F-104G; one General Electric J79-GE-11A turbojet of 15600/10000 lb thrust; |
1328 (M= 2.0) at h=35 000 |
860 (M= 1.13) at h=0 |
- |
48 000 |
- |
50 000 |
1875 |
3.37 |
0.0172 |
9.2 |
2/7/54 |
Republic F-105D; one Pratt & Whitney J75-P-19W turbojet of 24500/10000 lb thrust; |
1372 (M= 2.08) at h=36 090 |
836 (M= 1.1) at h=0 |
584 |
38500 |
1.7 (h=35000) |
49 600 |
2 207 |
6.65 |
0.0173 |
10.4 |
10/22/55 |
Vought F-8H; one Pratt & Whitney J57-P-420 turbojet of 16000/12400 lb thrust; |
1 156 (M= 1.75) at h=36 100 |
762 (M= 1.0) at h=0 |
556 |
23 300 |
- |
51000 |
1427 |
5.0 |
0.0133 |
12.8 |
3/25/55 |
McDonnell F-4E; two General Electric J79-GE-17 turbojets of 17900/11110 lb thrust each; |
1 486 (M= 2.25) at h=40 000 |
914 (M= 1.2) at h=0 |
586 |
54 200 |
- |
59 200 |
1885 |
11.87 |
0.0224 |
8.58 |
5/27/58 |
Northrop F-5E; two General Electric J85-GE-21 turbojets of 5000/3500 lb thrust each; |
997 (M= 1.51) at h=36 090 |
843 (M= 1.17) at h=0 |
- |
28 536 |
- |
53 800 |
1353 |
3.4 |
0.0200 |
10.0 |
7/30/59 |
General Dynamics F-111D; two Pratt & Whitney TF30-P-9 turbofans of 20840/12430 lb thrust each; |
1 453 (M= 2.2) at h=50 100 |
914 (M= 1.2) at h=0 |
500 |
25 800 |
- |
53 400 |
3298 |
9.36 |
.0186 |
15.8 |
12/21/64 |
Grumman F-14A; Two Pratt & Whitney TF30-P-412A turbofans of 20000/12500 lb thrust each; |
1 584 (M= 2.4) at h=49 000 |
913 (M= 1.2) at h=0 |
- |
- |
2.1 (h=60 000) |
- |
- |
- |
- |
- |
12/21/70 |
McDonnell Douglas F-15C; Two Pratt & Whitney F100-PW-100 turbofans of 23904/14780 lb thrust each; |
1 676 (M= 2.54) at h=40 000 |
922 (M= 1.21) at h=0 |
- |
- |
- |
63 000 |
3570 |
- |
- |
- |
7/27/72 |
General Dynamics F-16A; One Pratt & Whitney F100-PW-200 turbofans of 23830/14800 lb thrust each; |
1333 (M= 2.02) at h=40 000 |
- |
- |
- |
- |
- |
2535 |
- |
- |
- |
1/20/74 |
British Aerospace Harrier AV-8A; one Rolls-Royce Pegasus 103 turbofan of 21500 lb thrust; |
- |
720 (M= 0.95) at h=1 000 |
- |
- |
2.38 (h= 40 000) |
48 000 |
2070 |
- |
- |
- |
10/21/60 |
|
Aircraft;
engine; and references |
b |
|
S |
A |
|
Wg |
Wp |
We |
T/Wg |
Wg/S |
---|---|---|---|---|---|---|---|---|---|---|
North American B-45C; four General Electric J47-GE-13 turbojets of 5200 lb thrust each; |
89.0 |
75.5 |
1175 |
6.74 |
0 |
110 050 |
10 000 |
48 969 |
0.19 |
93.7 |
Boeing B-47E; six General Electric J47-GE-25 turbojets of 7200/5970 lb thrust each; |
116.0 |
107.1 |
1428 |
9.42 |
35 |
198 180 |
10 845 |
80 756 |
0.22 |
138.8 |
Boeing B-52H; eight Pratt & Whitney turbofans of 17000 lb thrust each; |
185.0 |
156.0 |
4000 |
8.56 |
35 |
488 000 |
10 000 |
169 822 |
0.28 |
112.5 |
Convair B-58A; four General Electric J79-GE-5B turbojets of 15500/10300 lb thrust each; |
56.8 |
96.8 |
1542 |
2.09 |
d 60 |
163 000 |
- |
55 560 |
0.38 |
105.7 |
Martin YP6M-1; four Allison J71-A-6 turbojets of 13000/9500 lb thrust each; b 200. |
102.5 |
134.3 |
1900 |
5.53 |
40 |
167 011 |
30 000 |
84 685 |
0.31 |
87.9 |
Rockwell International B-1A; four General Electric F101-GE-100 turbofans of 30000/16975 lb thrust each; |
c 136.8/78.1 |
150.1 |
1950 |
c 9.85/3.13 |
c 15/67.5 |
389 000 |
- |
- |
0.30 |
202.6 |
Martin B-57B; two Wright J65-W-5 turbojets of 7200 lb thrust each; |
64.0 |
65.5 |
960 |
4.27 |
0 |
53 721 |
5 240 |
27 091 |
0.27 |
56.0 |
Douglas A-4E; one Pratt & Whitney J52-P-6A turbojet of 8500 lb thrust; |
27.5 |
41.3 |
260 |
2.91 |
33 |
18 311 |
2 040 |
9 624 |
0.46 |
70.4 |
Grumman A-6E; two Pratt & Whitney J52-P-8A turbojets of 9300 lb thrust each; |
53.0 |
54.8 |
529 |
5.31 |
25 |
54 393 |
2 080 |
25 980 |
0.34 |
102.8 |
Vought A-7D; one Allison TF41-A-1 turbofan of 14250 lb thrust; |
38.8 |
46.1 |
375 |
4.00 |
35 |
38 008 |
6 560 |
19 733 |
0.38 |
101.4 |
Fairchild-Republic A-10A; two General Electric TF34-GE-100 turbofans of 9065 lb thrust each; 200. |
57.5 |
53.3 |
506 |
6.53 |
0 |
40 269 |
9 540 |
19 856 |
0.45 |
79.6 |
|
Aircraft;
engine; and references |
High Altitude |
Vmax Low Altitude |
|
|
|
|
|
|
|
|
|
|
---|---|---|---|---|---|---|---|---|---|---|---|---|
North American B-45C; four General Electric J47-GE-13 turbojets of 5200 lb thrust each; |
509 (M= 0.76) at h=32 500 |
573 (M=0.75) at h=0 |
466 |
153 |
- |
- |
1 008 |
2 426 |
18.80 |
f 0.0160 |
f 16.3 |
3/17/47 |
Boeing B-47E; six General Electric J47-GE-25 turbojets of 7200/5970 lb thrust each; |
557 (M= 0.84) at h=38 550 |
607 (M= 0.85) at h=16 300 |
498 |
175 |
4 660 |
40 500 |
2 013 |
4 035 |
21.13 |
f 0.0148 |
f 20.0 |
12/17/47 |
Boeing B-52H; eight Pratt & Whitney turbofans of 17000 lb thrust each; |
639 (M= 0.91) at h=20 700 |
- |
525 |
169 |
6 990 |
47 200 |
4 480 |
10 145 |
47.60 |
f 0.0119 |
f,g 21.5 |
4/15/52 |
Convair B-58A; four General Electric J79-GE-5B turbojets of 15500/10300 lb thrust each; |
1321 (M= 2.0) at h=63 150 |
700 (M= 0.92) at h=0 |
610 |
- |
17 830 |
64 800 |
1 500 |
4 025 |
10.49 |
0.0068 |
h 11.3 |
11/11/56 |
Martin YP6M-1; four Allison J71-A-6 turbojets of 13000/9500 lb thrust each; b 200. |
646 (M= 0.86) at h=5 000 |
- |
540 |
145 |
3 550 |
35 000 |
800 |
f 3 500 |
- |
- |
- |
7/14/55 |
Rockwell International B-1A; four General Electric F101-GE-100 turbofans of 30000/16975 lb thrust each; |
1452 (M= 2.2) at h=50 000 |
648 (M= 0.85) at h=50 000 |
- |
- |
- |
- |
- |
- |
- |
- |
- |
12/23/74 |
Martin B-57B; two Wright J65-W-5 turbojets of 7200 lb thrust each; |
- |
598 (M= 0.79) at h=2 500 |
476 |
124 |
6 180 |
45 100 |
948 |
2 722 |
11.45 |
0.0119 |
15.0 |
7/20/53 |
Douglas A-4E; one Pratt & Whitney J52-P-6A turbojet of 8500 lb thrust; |
- |
673 (M= 0.88) at h=0 |
498 |
139 |
- |
40 050 |
680 |
2 130 |
- |
- |
- |
6/22/54 |
Grumman A-6E; two Pratt & Whitney J52-P-8A turbojets of 9300 lb thrust each; |
- |
653 (M= 0.86) at h=0 |
390 |
142 |
- |
40 000 |
890 |
3 300 |
7.64 |
0.0144 |
15.2 |
4/19/60 |
Vought A-7D; one Allison TF41-A-1 turbofan of 14250 lb thrust; |
663 (M= 0.89) at h=7000 |
654 (M= 0.86) at h=0 |
507 |
174 |
- |
38 800 |
556 |
3 045 |
- |
- |
- |
9/27/65 |
Fairchild-Republic A-10A; two General Electric TF34-GE-100 turbofans of 9065 lb thrust each; 200. |
460 (M= 0.63) at h=10000 |
448 (M= 0.59) at h=0 |
329 |
120 |
6 200 |
37 800 |
e 288 |
3 510 |
- |
- |
- |
5/10/72 |
|