Aircraft;
engine; and references |
b | S | A | Wg | WL | We | T/Wg | Wg/S | ||
---|---|---|---|---|---|---|---|---|---|---|
DeHavilland Comet 1A; 4 DH Ghost turbojets, each 5000-lb thrust; |
115 |
93 |
2015 |
6.6 |
20 |
115 000 |
- |
- |
0.17 |
57.1 |
Tupolev Tu-104B; 2 Mikulin turbojets, each 21 385-lb thrust; |
113.3 |
131.5 |
1975 |
6.5 |
40/37.5 |
167 551 |
141 096 |
93 696 |
0.26 |
84.8 |
Boeing 367-80; 4 Pratt & Whitney JT3C turbojets, each 10 000-lb thrust; 126. |
129.8 |
127.8 |
2400 |
7.0 |
35 |
190 000 |
- |
92 120 |
0.21 |
79.2 |
Boeing 707-320B; 4 Pratt & Whitney JT3D-7 turbofans, each 19 000-lb thrust; |
145.8 |
152.8 |
3010 |
7.1 |
35 |
336 000 |
247 000 |
147 000 |
0.23 |
111.6 |
McDonnell Douglas DC-8 Super 63; 4 Pratt & Whitney JT3D-7 turbofans, each 19 000-lb thrust; |
148.4 |
187.5 |
2926.8 |
7.5 |
30.6 |
358 000 |
245 000 |
158 300 |
0.21 |
122.3 |
Sud-Aviation Caravelle VI-R; 2 Rolls-Royce Avon turbojets, each 12 000-lb thrust; |
112.5 |
105 |
1579 |
8.0 |
20 |
114 640 |
104 990 |
59 985 |
0.21 |
72.6 |
Boeing 727-200; 3 Pratt & Whitney JT8D-17 turbofans, each 16 000-lb thrust; |
108 |
153.2 |
1650 |
7.1 |
32 |
210 000 |
160 000 |
103 000 |
0.23 |
127.3 |
McDonnell Douglas DC-9-30; 2 Pratt & Whitney JT8D-15 turbofans, each 15 500-lb thrust; |
93.3 |
119.3 |
1001 |
8.7 |
24.5 |
109 000 |
99 000 |
56 000 |
0.28 |
108.9 |
Boeing 737-200; 2 Pratt & Whitney JT8D-17 turbofans, each 16 000-lb thrust; |
93 |
100 |
980 |
8.8 |
25 |
117 500 |
105 000 |
60 980 |
0.27 |
119.9 |
British Aircraft Corporation VC-10; 4 Rolls-Royce Conway RC042 turbofans, each 21 000-lb thrust; 127, 131. |
142.2 |
158.8 |
2932 |
6.9 |
32.5 |
314 000 |
216 000 |
146 979 |
0.27 |
107.1 |
Boeing 747-200B; 4 Pratt & Whitney JT9D-7R4G2 turbofans, each 54 750-lb thrust; |
195.8 |
231 |
5500 |
7.0 |
37.5 |
836 000 |
564 000 |
382 130 |
0.26 |
152 |
Lockheed L-1011-200; 3 Rolls-Royce RB.211-524 turbofans, each 48 000-lb thrust; |
155.3 |
177.7 |
3456 |
7.0 |
35 |
468 000 |
368 000 |
245 800 |
0.31 |
135.4 |
McDonnell Douglas DC-10-30; 3 General Electric CF6-50C1 turbofans, each 52 500-lb thrust; |
165.3 |
181.6 |
3647 |
7.5 |
35 |
575 000 |
403 000 |
261 459 |
0.27 |
158 |
Boeing 767-200; 2 Pratt & Whitney JT9D-7R4E turbofans, each 50 000-lb thrust; |
156.1 |
159..2 |
3050 |
8.0 |
31.5 |
337 000 |
278 000 |
180 230 |
0.30 |
111 |
Boeing 757-200; 4 Pratt & Whitney PW2037 turbofans, each 38 200-lb thrust; |
124.5 |
155.3 |
1951 |
7.9 |
25 |
241 000 |
198 000 |
128 050 |
0.32 |
123.5 |
Lockheed C-5A; 4 General Electric TF-39 turbofans, each 41 000-lb thrust; 129. |
222.8 |
247.8 |
6200 |
8.0 |
25 |
769 000 |
635 850 |
- |
0.21 |
124 |
Aircraft;
engine; and references |
Vc | Vce | Vs | Maximum payload range a | Full fuel tanks range a | lTb | lLb | Number of passengers | First flight |
---|---|---|---|---|---|---|---|---|---|
DeHavilland Comet 1A; 4 DH Ghost turbojets, each 5000-lb thrust; |
490 (M=0.74) at h=35 000 |
- |
- |
1 750 |
- |
- |
- |
44 |
7/27/49 |
Tupolev Tu-104B; 2 Mikulin turbojets, each 21 385-lb thrust; |
590 (M=0.85) at h=25 000 |
497 (M=0.75) at h=35 000 |
127 |
e 1 500 (Wp=26 455) |
2 214 (Wp=13 225) |
f 7 220 |
f 6 070 |
100 |
6/17/55 |
Boeing 367-80; 4 Pratt & Whitney JT3C turbojets, each 10 000-lb thrust; 126. . |
550 |
- |
- |
(Wp=25 000) |
- |
- |
- |
- |
7/15/54 |
Boeing 707-320B; 4 Pratt & Whitney JT3D-7 turbofans, each 19 000-lb thrust; |
593 (M=0.87) at h=30 000 |
550 (M=0.83) at h=35 000 |
121 |
6 240 (Wp=53 900) |
7 975 (Wp=33350) |
10 000 |
6 250 |
189 |
1959 |
McDonnell Douglas DC-8 Super 63; 4 Pratt & Whitney JT3D-7 turbofans, each 19 000-lb thrust; |
596 (M=0.87) at h=29 000 |
544 (M=0.82) at h=35 000 |
123 |
4 882 (Wp=67 735) |
6 997 (Wp=37 101) |
10 440 |
5 900 |
259 |
1958 |
Sud-Aviation Caravelle VI-R; 2 Rolls-Royce Avon turbojets, each 12 000-lb thrust; |
526 (M=0.76) at h=25 000 |
488 (M=0.74) at h=35 000 |
- |
1 829 (Wp=16 800) |
- |
6 750 |
5 650 |
80 |
5/27/55 |
Boeing 727-200; 3 Pratt & Whitney JT8D-17 turbofans, each 16 000-lb thrust; |
610 (M=0.88) at h=25 000 |
549 (M=0.82) at h=33 000 |
121 |
3 335 (Wp=41 000) |
3 738 (Wp=36 000 |
9 950 |
4 900 |
189 |
1963 |
McDonnell Douglas DC-9-30; 2 Pratt & Whitney JT8D-15 turbofans, each 15 500-lb thrust; |
578 (M=0.84) at h=26 000 |
522 (M=0.78) at h=33 000 |
120 |
1 812 (Wp=31 000) |
2 210 (Wp=27 527) |
6 200 |
4 700 |
115 |
1965 |
Boeing 737-200; 2 Pratt & Whitney JT8D-17 turbofans, each 16 000-lb thrust; |
564 (M=0.81) at h=25 000 |
501 (M=0.75) at h=33 000 |
116 |
1 748 (Wp=34 000) |
3 082 (Wp=21 750) |
6 475 |
4 430 |
130 |
1967 |
British Aircraft Corporation VC-10; 4 Rolls-Royce Conway RC042 turbofans, each 21 000-lb thrust; |
568 |
550 (M=0.83) at h=38 000 |
138 |
5 040 (Wp=39 769) |
- |
8 280 |
6 380 |
151 |
6/29/62 |
Boeing 747-200B; 4 Pratt & Whitney JT9D-7R4G2 turbofans, each 54 750-lb thrust; |
583 |
564 (M=0.85) at h=35 000 |
125 |
6 854 (Wp=144 520) |
8 706 (Wp=87 800) |
10 450 |
6 150 |
550 |
2/9/69 |
Lockheed L-1011-200; 3 Rolls-Royce RB.211-524 turbofans, each 48 000-lb thrust; |
607 (M=0.90) at h=31 000 |
567 (M=0.84) at h=31 000 |
125 |
4 884 (Wp=74 200) |
6 204 (Wp=42 827) |
8 070 |
5 820 |
400 |
11/16/70 |
McDonnell Douglas DC-10-30; 3 General Electric CF6-50C1 turbofans, each 52 500-lb thrust; |
593 (M=0.88) at h=31 000 |
574 (M=0.85) at h=31 000 |
- |
4 853 (Wp=106 541) |
6 296 (Wp=65 175) |
10 370 |
5 830 |
386 |
8/70 |
Boeing 767-200; 2 Pratt & Whitney JT9D-7R4E turbofans, each 50 000-lb thrust; |
557 (M=0.84) at h=39 000 |
528 (M=0.80) at h=39 000 |
122 |
4 111 (Wp=72 770) |
5 992 (Wp=42 545) |
7 000 |
4 850 |
290 |
9/81 |
Boeing 757-200; 4 Pratt & Whitney PW2037 turbofans, each 38 200-lb thrust; |
561 (M=0.83) at h=30 000 |
593 (M=0.80) at h=39 000 |
117 |
3 749 (Wp=56 050) |
5 290 (Wp=36 900) |
7 370 |
4 600 |
239 |
2/82 |
Lockheed C-5A; 4 General Electric TF-39 turbofans, each 41 000-lb thrust; 129. |
541 (M=0.78) at h=25 000 |
- |
120 |
3 744 (Wp=220 967) |
6 521 (Wp=112 600) |
f 8 400 |
f 3 600 |
- |
6/30/68 |
Aircraft;
engine; and references |
b | S | A | Wg | WL | We | T/Wg | Wg/S | ||
---|---|---|---|---|---|---|---|---|---|---|
Lockheed JetStar; 4 Pratt & Whitney JT-12-8 turbojets, each 3300-lb thrust; |
54.5 |
60.5 |
542.5 |
5.3 |
30 |
42 500 |
35 000 |
21 676 |
0.31 |
78.3 |
Gates Learjet 24B; 2 General Electric CJ610-4 turbojets, each 2850-lb thrust; 127. |
35.5 |
43.3 |
231.8 |
5.4 |
13 |
13 300 |
11 880 |
6 700 |
0.43 |
57.4 |
Gates Learjet 55; 2 AiResearch TFE 731-3 turbofans, each 3650-lb thrust; |
43.8 |
55.1 |
264.5 |
7.3 |
13 |
19 500 |
17 000 |
12 130 |
0.37 |
73.7 |
Dassault-Breguet Falcon 20; 2 General Electric CF700 turbofans, each 4315-lb thrust; |
53.5 |
56.3 |
440 |
6.5 |
30 |
28 660 |
- |
15 970 |
0.30 |
65.1 |
Gulfstream Aerospace Gulfstream II; 2 Rolls-Royce Spey Mk 511-8 turbofans, each 11 400-lb thrust; |
68.8 |
79.9 |
793.5 |
6.0 |
25 |
62 500 |
58 500 |
37 186 |
0.56 |
79 |
Cessna Citation II; 2 Pratt & Whitney JT15D-4 turbofans, each 2500-lb thrust; |
51.8 |
47.2 |
323 |
8.3 |
0 |
13 300 |
12 700 |
7 181 |
0.38 |
41.2 |
Cessna Citation III; 2 AiReseach TFE 731-3 turbofans, each 3650-lb thrust; |
53.3 |
55.5 |
312 |
9.11 |
25 |
20 000 |
16 500 |
10 951 |
0.37 |
64.31 |
MBB HFB Hansa; 2 General Electric CJ610-1 turbojets, each 2850-lb thrust; |
47.5 |
54.5 |
324.4 |
7.0 |
-15 |
18 740 |
17 860 |
10 670 |
0.31 |
57.8 |
Aircraft;
engine; and references |
Vc | Vce | Vs | Maximum payload range a | Full fuel tanks range a | lTb | lLb | Number of passengers | First flight |
---|---|---|---|---|---|---|---|---|---|
Lockheed JetStar; 4 Pratt & Whitney JT-12-8 turbojets, each 3300-lb thrust; |
567 (M= 0.80) at h = 21 000 |
520 |
122 |
2415 (Wp=3500) |
- |
c 4 700 |
c3 550 |
8 to 10 |
9/9/57 |
Gates Learjet 24B; 2 General Electric CJ610-4 turbojets, each 2850-lb thrust; 127. |
534 (M= 0.81) at h = 41 000 |
508 (M= 0.77) at h = 41 000 |
104 |
1271 (Wp=1910) |
2041 |
3 100 |
3 350 |
6 |
10/7/63 |
Gates Learjet 55; 2 AiResearch TFE 731-3 turbofans, each 3650-lb thrust; |
505 (M= 0.76) at h = 45 000 |
461 (M= 0.70) at h = 49 000 |
113 |
- |
2 489 (4 passengers) |
4 950 |
3 109 |
6 to 10 |
4/19/79 |
Dassault-Breguet Falcon 20; 2 General Electric CF700 turbofans, each 4315-lb thrust; |
535 (M= 0.77) at h = 25 000 |
466 (M= 0.70) at h = 40 000 |
94 |
- |
2 220 (Wp=1600) |
4 750 (Wg= 27 130) |
3 220 |
8 to 10 |
7/10/64 |
Gulfstream Aerospace Gulfstream II; 2 Rolls-Royce Spey Mk 511-8 turbofans, each 11 400-lb thrust; |
588 (M= 0.85) at h = 25 000 |
503 (M= 0.76) a t h = 43 000 |
128 |
- |
3881 |
5 000 |
3 190 |
10 to 14 |
10/2/66 |
Cessna Citation II; 2 Pratt & Whitney JT15D-4 turbofans, each 2500-lb thrust; |
443 (M= 0.64) at h = 25 000 |
- |
94 |
- |
1969 (6 passengers) |
2 990 |
2 270 |
6 to10 |
9/16/69 |
Cessna Citation III; 2 AiReseach TFE 731-3 turbofans, each 3650-lb thrust; |
539 (M= 0.81) at h = 33 000 |
- |
104 |
2875 |
(6 passengers) |
4 510 |
2 770 |
Maximum of 13 |
5/30/79 |
MBB HFB Hansa; 2 General Electric CJ610-1 turbojets, each 2850-lb thrust; |
509 (M= 0.74) at h = 26 000 |
449 (M= 0.68) at h = 39 000 |
101 |
949 (Wp=2650) |
1668 (Wp=1760) |
4 650 |
2 900 |
9 or 10 |
4/64 |