i think a f-15 eagle would lose in a fight with such a great plane. the f-15 is a great plane but i think the foxhound would decimate it in a
dogfight.
now don't get me wrong im for america but i think the russians are catching up in fighter technology and they might have planes equal or superior to
the raptor.
General Characteristics
Primary function: Tactical fighter
Contractor: McDonnell Douglas Corp.
Power plant: Two Pratt & Whitney F100-PW-100, 220 or 229 turbofan engines with afterburners
Thrust: (C/D models) 23,450 pounds each engine
Wing span: 42.8 feet (13 meters)
Length: 63.8 feet (19.44 meters)
Height: 18.5 feet (5.6 meters)
Speed: 1,875 mph (Mach 2.5 plus)
Maximum takeoff weight: (C/D models) 68,000 pounds (30,844 kilograms)
Ceiling: 65,000 feet (19,812 meters)
Range: 3,450 miles (3,000 nautical miles) ferry range with conformal fuel tanks and three external fuel tanks
Crew: F-15A/C: one. F-15B/D/E: two
Armament: One internally mounted M-61A1 20mm 20-mm, six-barrel cannon with 940 rounds of ammunition; four AIM-9L/M Sidewinder and four AIM-7F/M
Sparrow air-to-air missiles, or eight AIM-120 AMRAAMs, carried externally.
Unit Cost: A/B models - $27.9 million (fiscal 98 constant dollars);C/D models - $29.9 million (fiscal 98 constant dollars)
Date deployed: July 1972
Inventory: Active force, 396; Reserve, 0; ANG,126.
Countries of Origin CIS (formerly USSR)
Similar Aircraft MiG-25 Foxbat
F-14 Tomcat
F-15 Eagle
Crew Two
Role interceptor
air superiority
Length 70 ft, 5 in (21.5 m)
Span 45 ft, 9 in (14 m)
Height: 6.60 m
Wing span: 14.02 m
Wing area: 61.41 sq m
Maximum speed: Mach 2.83
Weight: (empty) 22,000 kg
Weight: (normal) 36,720 kg
Powerplant: Two Tumanski R-15BD-300
afterburning turbojets rated at
49.78kN each
Maximum Range: 1,250 km
Service ceiling: 20,700 m
Rate of climb: 8 min 54 sec to 20,000 m
Ceiling 24400 meters
Cruise range 1620 nm
In-Flight Refueling No
Internal Fuel 14200kg
Drop Tanks 2000L drop tank with 1600kg of fuel for 91 nm range
Sensors LD/SD TWS radar, possible IRST, RWR
Armament cannon
R-33 AA-9 Amos
AA-11 Archer
Typically
two R-40 missiles
Four R-60 missiles
ESTIMATED COST:
$133 million [2005$]
AIRFOIL SECTIONS:
Wing Root NACA 64A?05.92
Wing Tip
NACA 64A?04.29
DIMENSIONS:
Length 62.08 ft (18.92 m)
Wingspan 44.50 ft (13.56 m)
Height 16.42 ft (5.00 m)
Wing Area 838 ft2 (78.0 m2)
Canard Area
not applicable
WEIGHTS:
Empty 34,000 lb (15,420 kg)
Typical Load 60,000 lb (27,215 kg)
Max Takeoff 62,000 lb (28,125 kg)
Fuel Capacity internal: 25,000 lb (11,340 kg)
external: 16,035 lb (7,290 kg) in four 600 gal (2,270 L) tanks
Max Payload
3,915 lb (1,775 kg) [internal]
approximately 19,000 lb (8,635 kg) [external]
PROPULSION:
Powerplant two Pratt & Whitney F119-100 afterburning turbofans
Thrust 70,000 lb (310 kN)
PERFORMANCE:
Max Level Speed at altitude: 1,355 mph (2,180 km/h) at 30,000 ft (9,150 m), Mach 2 [afterburner]
1,070 mph (1,725 km/h) at 30,000 ft (9,150 m), Mach 1.58 [supercruise]
at sea level: 920 mph (1,480 km/h), Mach 1.2
Initial Climb Rate unknown
Service Ceiling 50,000 ft (15,240 m)
Range typical: 2,000 nm (3,700 km)
ferry: unknown
Endurance unknown
g-Limits +9.0 / -3.0
ARMAMENT:
Gun one 20-mm M61A2 Vulcan cannon (480 rds)
Stations four internal weapons bays and four external hardpoints
Air-to-Air Missile AIM-9M Sidewinder, AIM-120A/C AMRAAM
AIM-9X Sidewinder planned
Air-to-Surface Missile none at present
possibly AGM-158 JASSM in the future
Bomb GBU-32 JDAM
GBU-39 Small Diameter Bomb planned
Other unknown
[edit on 29-7-2005 by Karl Toussaint]