Please tell me all the data and information of the F A 22 fighter Thank you

Updated on military 2024-03-19
5 answers
  1. Anonymous users2024-02-06

    F-22 fighter data:

    Crew: 1 person.

    Length: m. Wingspan: m.

    Height: m. Wing area: square meters.

    Empty weight: 19700 kg.

    Maximum take-off weight: 38000 kg.

    Power system: 2 Pratt & Whitney F119-PW-100 turbofan engine thrust: maximum thrust: 2 104 kN; Afterburner thrust: 2 156 kN.

    F-22 Fighter Performance:

    Maximum flight speed: Mach (1500 mph, 2410 kmh) Ceiling: 19812 m.

    Range: 1600 nautical miles (2963 km).

    Combat radius: 410 nautical miles (759 km).

    Wing load: 375 kg sqm.

    Thrust-to-weight ratio: limit overload:

    **System: Main**: 4 external hardpoints, 2 built-in bomb bays (bomb load 2270 kg), air-to-air loading of 6 AIM-120 + 2 AIM-9 missiles; Auxiliary**:

    1 x 20 mm M61A2 Vulcan cannon with 480 rounds of ammunition.

  2. Anonymous users2024-02-05

    F-22 fighter (English: F-22 Fighter, designation: F-22, code name Nickname:

    Raptor, commonly known as: Lockheed Martin F-22 "Raptor"), is an American single-seat twin-engine high-stealth fifth-generation fighter, and is the world's first fifth-generation fighter to enter service.

    The combination of stealth performance, agility, accuracy and situational awareness of the F-22 fighter, combined with its air-to-air and air-to-ground combat capabilities, makes it the best comprehensive fighter in the world today.

  3. Anonymous users2024-02-04

    Overall length: meters.

    Overall height: m.

    Wingspan: m.

    Wing area: square meters.

    Empty weight: 16,000 kg (latest estimate).

    Full take-off: 35,000 kg.

    Fuel inside: Confidential, 14375L

    Load: 2270 kg (fully loaded).

    Load: 9000 kg (including plug-in, up to 12tons) body material weight ratio: 42% titanium alloy, 23% composite materials, 15% aluminum alloy, 20% others.

    Ceiling: 18,288 meters.

    Controllable angle of attack maneuvering: more than plus or minus 60 degrees.

    Actual supersonic cruise speed: Mach (15% more than the YF22 indicator) Maximum speed: Mach.

    Acceleration capability: 54 seconds (2% more than the YF22 indicator).

    Rate of sea level climb: 350 m sec or more.

    Maximum G Limit: 3G +9G (Human Normal Operation Limit) Instantaneous Circling Angle Rate: 30 degrees per second.

    Acceleration capability: (from 200 knots to Mach 1) Less than 30 seconds.

  4. Anonymous users2024-02-03

    Crew: 1 person.

    Number of engines: 1 unit.

    Maximum take-off weight: tons.

    Captain: m. Wingspan: m.

    Machine height: meters. Engine thrust: kN.

    Afterburner thrust: kN.

    Combat radius: 834 km.

    Dimensions. Wingspan (including wingtip missile slides) meters.

    Aspect ratio leading edge sweep angle 33°12'

    Wing area m2

    Main track meters.

    Front and rear track meters.

    Weight and load.

    Empty weight 9527 kg.

    Maximum internal fuel 3602 kg.

    Maximum external fuel 4422 kg.

    Design maximum take-off weight (with plug-in) 22,100 kg, designed maximum landing weight 18,300 kg.

    Maximum wing load kg m2

    Maximum power load 168 kg kN.

    Performance data. Maximum level flight speed.

    High altitude approx. Low altitude combat radius (carries 4 anti-ship missiles, 2 air-to-air missiles.

    and 2 auxiliary fuel tanks of 2272L for anti-ship missions) > 834 km design limits overload.

    The take-off weight is 12000 kg +9 -3g

    Maximum take-off weight +

  5. Anonymous users2024-02-02

    Reference data Length m Wingspan m Height m Empty weight 5,980 kg Maximum take-off weight 11,437 kg Engine 2 Westinghouse J34-We-34 turbofan Thrust 2 kN Reference performanceMaximum speed 933 km/h climb rate 30 m Practical ceiling 14,205 m Maximum range 2,760 km Airborne armament Cannon 4 20 mm (inch) Colt MK 16 cannon Miscellaneous 2 AIM-9 Sidewinder missiles.

    8 60-pound high-explosive rockets.

    6 500 pounds of bombs.

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