Data on Modern Fighter Aircraft.

Sources:

1. The Aircraft Gallery: http://www.geocities.com/CapeCanaveral/8585/

2. Data found by the students in AE1350, Introduction to Aerospace Engineering, at the School of Aerospace Engineering, Georgia Institute of Technology, in Fall 1999, from various sources.
 
 
F-22 F-15  MiG-29 Su-27  Sukhoi 30MK Su-35  Sukhoi 37 JSF Gripen JAS39 Mirage 2000 Tornado Eurofighter 2000 Rafale SR-71
Year commissioned 2000? 1979 1984
T.O.W., lbs 60000 68000 40,875 66138  66,138  74956 27560 / 28660 37478 46297 54013
#of engines 2-F119PW100  2-F100PW229  2-Sarkisov RD-33 2-Lyulka AL-35  2  2 1 1-F404-GE400 / Volvo Flymotor RM12  1-SNECMA M53-P2 2-Eurojet EJ2000 2
Max dry thrust 35600 22220  lb  18739? 12140 14460 26980 21900
Max wet thrust 70000lb  58200 36600 55114  27,557  30885? 18100 21835 40500 32800
Wing Area, sq.ft 840 or 830?  609 409  538.15  500 (model220-c) 441.3 538 491.9
W/S; psf 71.42 92.105  102 (or 112.32?)psf 109.8psf
Span b 44.5 ft 42' 9.5" 37'3.5" 48'2.5" 27' 27.5" 34'5.5"
length 62ft. 1inch 63'9" 56' 10" 71'11.5" 46' 3" 47' 7"
height 18' 5.5" 15' 6.5" 19' 5.5" 14' 9"
Wing LE Sweep 42 deg. 38 deg 42 min ? 47 deg 50'; 73 deg30'?   35 58 53 deg. 
# vert. tails  2 2  2  2  2 2 2
WingTEsweep 17 deg. (tapered)
Max speed  1482 mph; Mach 1.7* 
Mach 2.3
 1665 mph/Mach 2.5* 
1875mph
 1520 mph* 
Mach 2.3; Mach 3 at ceiling; M=1.225 at sealevel
1553: Mach 2.35  1553mph  1516mph 1329mph 1461 mph 1321mph Mach 1.8
% composite 28
Takeoff Distance 2625ft.  1640 feet
Ceiling, ft. 50,000  65,000  55,775 59,055  59,055  59,055 56000 55,000
Range   3,450 miles  1300 miles  1064 miles  2175 miles 1875 miles 2084
Rate of Climb  50000fpm 64,960 ft/min.    45275 ft/min. 60000ft/min 60000ft/min
 Armament 1-M162 20mm cannon; 

2JDAM; 4-AIM-9, 
4-AIM-120AMARAAMs 

3-AIM-9M Sidewinders or AIM-120C AMRAAMs and/or 460kg GBU-32 JDAMs

1-20mm cannon; 8 AAM 1-20mm M61A1 Vulcan 6-barrel cannon with 940 rounds; up to 23,600lbs) of ordinance can include: nuclear weapons, ASMs, AAMs, free-fall or guided bombs, cluster bombs, dispenser weapons, rocket launchers, napalm tanks, drop tanks and ECM pods, carried on 9 external hardpoints.
    One 30mm GSh-30-1 cannon with 150 rounds; up to 3,000 kilograms (6,614 pounds) of ordinance can include: AAMs, ASMs, free-fall or guided bombs, cluster bombs, dispenser weapons, rocket launchers, drop tanks and ECM pods, carried on six external hardpoints. 

    1-30mm cannon; 6614lbs bombs and missiles

    One 30mm GSh-30-1 cannon with 149 rounds; up to 8,165 kilograms (18,000 pounds) of ordinance can include: AAMs, free-fall bombs, rocket launchers, drop tanks and ECM pods, carried on 10 external hardpoints.
 1-30mm cannon, 13228lbs bombs & missiles  1-30mm cannon, 18075lbs bombs & missiles 2 AIM-120, AMRAAMs, 2-1000lbJDAM bombs One Mauser BK27 27mm cannon, up to 6,500 kilograms (14,330 pounds) of ordinance can include: Rb15F and Rb75 ASMs, DWS 39 munitions dispensers, air-to-surface rockets, free-fall/retarded bombs, Rb74 and AIM-120 AAMs, recce/sensor pods, auxilary fuel tanks. 2-30mm DEFA 554 cannon, 13890lb carried on 4 underwing and 5 under-fuselage hardpoints; incl. Matra Magic 2, Matra Super 530D AAMs, laser-guided bombs, iron bombs, cluster bombs, AS30L ASMs, Armat anti-radiation missiles, AM39 Excoet anti-ship missiles.  One Mauser Mk27 27mm cannon; up to 6,500 kilograms (14,330 pounds) of ordinance can include: AIM-120 AMRAAMs, Aspide AAMs, short-range AAMs, various air-to-surface weapons, three auxillary fuel tanks.
Max Payload; lbs 23000  20000 lbs 20337lbs  34391 lbs 13200 lbs 20944lbs
Crew 1 or 2 1 or 2  1 2 2  1 1
Conceived from the late 1960s as a high-performance fighter of the relaxed-stability type with a quadruplex analog fly-by-wire control system, the Su-27 was almost certainly the USSR's first genuine look-down/shoot-down fighter with its pulse-Doppler radar and up to 10 AAMs. The first of 15 'Flanker-A' prototypes flew on May 20, 1977, and was followed in April 1981 by the 'Flanker-B' initial production model that entered service in 1984 with squared-off wing tips carrying missile launch rails. The type also has a number of aerodynamic refinements such as vertical tail surfaces located farther outboard, an extended tailcone, and leading-edge flaps. The Su-27UB 'Flanker-C' is the tandem two-seat variant first revealed in 1989 with taller vertical tail surfaces. The variant has an improved radar in a slightly longer nose, and is probably as much of a combat type as a trainer, with the rear-seat officer managing of the warplane's upgraded avionics and weapon systems. 

The Su-27K 'Flanker-D' is the navalized version of the 'Flanker-B' selected in 1992 for deployment on the navy's new conventional aircraft carriers. This version has folding wings and tailplane halves, a retractable flight refueling probe, an arrestor hook under a shortened bullet fairing between the paired engine, strengthened landing gear, moving canard foreplanes to allow slower landing at higher angles of attack, and engine uprated some 12% to 15%."

130mm cannon and 14 stores