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Military Aircrafts: Designs and Concepts

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  • #11
    Re: Military Aircrafts: Designs and Concepts

    United States, Chance Vought F6U Pirate






    General characteristics

    Crew: 1
    Length: 37 ft 7 in (11.46 m)
    Wingspan: 32 ft 10 in (10 m)
    Height: 12 ft 11 in (3.39 m)
    Wing area: 203.4 ft² (18.9 m²)
    Empty weight: 7,320 lb (3,320 kg)
    Loaded weight: 12,900 lb (5,850 kg)
    Powerplant: 1 × Westinghouse J34-WE-30A turbojet
    Dry thrust: 3,150 lbf (14.0 kN)
    Thrust with afterburner: 4,224 lbf (18.78 kN)

    Performance

    Maximum speed: 596 mph (517 kn, 959 km/h)
    Range: 1,170 mi (1,020 nmi, 1,880 km)
    Service ceiling: 46,260 ft (14,100 m)
    Rate of climb: 8,060 ft/min (40.95 m/s)
    Wing loading: 63.4 lb/ft² (304 kg/m²)
    Thrust/weight: 0.327
    https://en.wikipedia.org/wiki/Vought_F6U_Pirate
    Last edited by Armynia; 12-29-2015, 01:01 PM.

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    • #12
      Re: Military Aircrafts: Designs and Concepts

      United States, Vought F7U-3 Cutlass






      General characteristics

      Crew: 1
      Length: 41 ft 3.5 in (12.586 m)
      Wingspan: 39 ft 8 in (12.1 m)
      Span wings folded: 22.3 ft (6.80 m)
      Height: 14 ft 0 in (4.27 m)
      Wing area: 496 sq ft (46.1 m2)
      Empty weight: 18,210 lb (8,260 kg)
      Gross weight: 26,840 lb (12,174 kg)
      Max takeoff weight: 31,643 lb (14,353 kg)
      Powerplant: 2 × Westinghouse J46-WE-8B after-burning turbojet engines, 4,600 lbf (20 kN) thrust each dry, 6,000 lbf (27 kN) with afterburner


      Performance

      Maximum speed: 606 kn (697 mph; 1,122 km/h) at sea level with Military power + afterburner
      Cruise speed: 490 kn (564 mph; 907 km/h) at 38,700 ft (11,796 m) to 42,700 ft (13,015 m)
      Stall speed: 112 kn (129 mph; 207 km/h) power off at take-off
      93.2 kn (173 km/h) with approach power for landing
      Combat range: 800 nmi (921 mi; 1,482 km)
      Service ceiling: 40,600 ft (12,375 m)
      Rate of climb: 14,420 ft/min (73.3 m/s) with Military power + afterburner
      Time to altitude: 20,000 ft (6,096 m) in 5.6 minutes
      30,000 ft (9,144 m) in 10.2 minutes
      Wing loading: 50.2 lb/sq ft (245 kg/m2)
      Thrust/weight: 0.45
      Take-off run: in calm conditions 1,595 ft (486 m) with Military power + afterburner
      https://en.wikipedia.org/wiki/Vought_F7U_Cutlass
      Last edited by Armynia; 12-29-2015, 01:03 PM.

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      • #13
        Re: Military Aircrafts: Designs and Concepts

        Thanks for sharing Armenian lion.........please don't stop.
        B0zkurt Hunter

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        • #14
          Re: Military Aircrafts: Designs and Concepts

          People's Republic of China, Chengdu J-10







          General characteristics

          Crew: 1[13]
          Length: 15.49 m (50.82 ft)
          Wingspan: 9.75 m (31.99 ft)
          Height: 5.43 m (17.81 ft)
          Wing area: 39 m² (356.3 ft²)
          Empty weight: 9,750 kg (21,495 lb)
          Loaded weight: 12,400 kg (28,600 lb)
          Useful load: 6,000 kg[55] (13,200lb)
          Max. takeoff weight: 19,277 kg (42,500 lb)
          Powerplant: 1 × Saturn-Lyulka AL-31FN or WS-10A turbofan
          Dry thrust: 79.43 kN / 89.17 kN (17,860 lbf / 19,000 lbf)
          Thrust with afterburner: 125 kN / 130 kN (27,999 lbf / 29,000 lbf)

          Performance

          Maximum speed: Mach 2.2 at altitude,[56][57] Mach 1.2 at sea level
          Combat radius: 550 km[55] (342 mi)
          Ferry range: 1,850 km[55] (1,150 mi)
          Service ceiling: 18,000 m[55] (59,055 ft)
          Wing loading: 381 kg/m² (78 lb/ft²)
          Thrust/weight: 1.15 (with AL-31FN3); 1.16 (with WS-10B)
          Maximum g-load: +9/–3 g
          https://en.wikipedia.org/wiki/Chengdu_J-10
          Last edited by Armynia; 12-29-2015, 01:05 PM.

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          • #15
            Re: Military Aircrafts: Designs and Concepts

            United States, Convair F-102 Delta Dagger






            General characteristics

            Crew: 1
            Length: 68 ft 4 in (20.83 m)
            Wingspan: 38 ft 1 in (11.61 m)
            Height: 21 ft 2 in (6.45 m)
            Wing area: 661.5ft²/61.52m² (Original Wing) or 695 ft²/64.57m² (Conically-Cambered Wing) ()
            Airfoil: NACA 0004-65 mod root and tip
            Empty weight: 19,350 lb (8,777 kg)
            Loaded weight: 24,500 lb (11,100 kg)
            Max. takeoff weight: 31,500 lb (14,300 kg)
            Powerplant: 1 × Pratt & Whitney J57-P-25 afterburning turbojet
            Dry thrust: 11,700 lbf (52.0 kN)
            Thrust with afterburner: 17,200 lbf (76.5 kN)
            Internal fuel capacity: 1,085 U.S. gal (4,107 l)
            External fuel capacity: 2 × 215 U.S. gal (815 l) drop tanks


            Performance

            Maximum speed: Mach 1.25 (825 mph, 1,304 km/h) at 40,000 ft (12,190 m)
            Range: 1,350 mi (1,170 nmo, 2,175 km)
            Service ceiling: 53,400 ft (16,300 m)
            Rate of climb: 13,000 ft/min (66 m/s)
            Wing loading: 35 lb/ft² (172 kg/m²)
            Thrust/weight: 0.70
            https://en.wikipedia.org/wiki/Convai...2_Delta_Dagger
            Last edited by Armynia; 12-29-2015, 01:07 PM.

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            • #16
              Re: Military Aircrafts: Designs and Concepts

              United States, Convair F-106 Delta Dart







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              • #17
                Re: Military Aircrafts: Designs and Concepts

                France, Dassault Mystere IV








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                • #18
                  Re: Military Aircrafts: Designs and Concepts

                  France, Dassault Mirage III






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                  • #19
                    Re: Military Aircrafts: Designs and Concepts

                    France, Dassault Mirage F-1







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                    • #20
                      Re: Military Aircrafts: Designs and Concepts

                      France, Dassault Mirage 2000






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