SAWE Report - Cal Poly San Luis Obispo
SAWE Report - Cal Poly San Luis Obispo
SAWE Report - Cal Poly San Luis Obispo
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Table 1.III - Comparison of the F-111, F-117, B-2, B-1B, and F-15E<br />
Manufacturer Lockheed<br />
General<br />
Dynamics<br />
Boeing Northrop Rockwell<br />
Type F-117 FB-111A F-15E B-2 B-1B<br />
b - ft<br />
(m)<br />
43.6<br />
(13.3)<br />
32.0<br />
(9.2)<br />
42.8<br />
(13.0)<br />
172.0<br />
(52.4)<br />
78.2<br />
(23.8)<br />
AR – – 3 – –<br />
L – ft<br />
(m)<br />
H – ft<br />
(m)<br />
Wing - ft 2<br />
(m 2 )<br />
W oe – lb<br />
(kg)<br />
W pl – lb<br />
(kg)<br />
W f – lb<br />
(kg)<br />
W to – lb<br />
(kg)<br />
66.6<br />
(20.3)<br />
12.5<br />
(3.8)<br />
913<br />
(84.8)<br />
29,500<br />
(133,801)<br />
5,000<br />
(2,267)<br />
73.5<br />
(22.4)<br />
17.1<br />
(5.21)<br />
–<br />
46,171<br />
(20,943)<br />
31,500<br />
(14,488)<br />
– –<br />
52,501<br />
(23,814)<br />
91,492<br />
(41,500)<br />
63.7<br />
(19.4)<br />
18.5<br />
(5.6)<br />
608<br />
(56.5)<br />
32,000<br />
(14,515)<br />
24,500<br />
(11,113)<br />
13,122<br />
(5,952)<br />
81,000<br />
(36,740)<br />
69.0<br />
(21)<br />
17.0<br />
(5.2)<br />
5274<br />
(490.0)<br />
153,700<br />
(69,717)<br />
40,001<br />
(18,144)<br />
200,003<br />
(90,720)<br />
375,998<br />
(170,550)<br />
147.0<br />
(44.8)<br />
34.0<br />
(10.4)<br />
1950<br />
(181.1)<br />
192,001<br />
(87,090)<br />
133,999<br />
(60,780)<br />
194,999<br />
(88,450)<br />
477,003<br />
(216,365)<br />
Max power loading – – 1.73 4.86 –<br />
Max level (Mach) 0.9 2.2 2.5 0 1.25<br />
Max combat radius<br />
nm<br />
Service Ceiling - ft<br />
(m)<br />
570 2,750 686 6,300 6,479<br />
–<br />
50,853<br />
(15,500)<br />
–<br />
50,000<br />
(15,240)<br />
The solution to the RFP is not a trivial one. The aircraft will have to be well area ruled and have<br />
a low frontal cross-section in order to minimize wave drag. The goal of this design is to meet or<br />
exceed RFP requirements while minimizing manufacturing and operating costs.<br />
–<br />
6
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