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,
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. |
1-30mm cannon; 6614lbs bombs and missiles |
|
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.
|
130mm cannon and 14 stores |