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Military Aircrafts: Designs and Concepts

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  • #41
    Re: Military Aircrafts: Designs and Concepts

    U.S. Lockheed/Martin F-80c Shooting Star






    Comment

    • #42
      Re: Military Aircrafts: Designs and Concepts

      U.S. Lockheed/Martin F-94b starfire







      Comment

      • #43
        Re: Military Aircrafts: Designs and Concepts

        U.K. Hawker Sea Hawk








        Last edited by Armynia; 12-26-2015, 11:33 AM.

        Comment

        • #44
          Re: Military Aircrafts: Designs and Concepts

          U.S. Lockheed/Martin F-104 Starfighter







          Last edited by Armynia; 12-29-2015, 12:17 PM.

          Comment

          • #45
            Re: Military Aircrafts: Designs and Concepts

            Deer friends if you are going to post in this aviation thread, Please provide the following if possible.

            Aircraft:

            1. Origin,Company and Name
            2. Cutaway and Blueprint
            3. Pictures
            Last edited by Armynia; 12-28-2015, 06:47 AM.

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            • #46
              Re: Military Aircrafts: Designs and Concepts

              Brazil, Embraer EMB 314 Super Tucano








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              • #47
                Re: Military Aircrafts: Designs and Concepts

                U.S. McDonnell FH-1 Phantom






                Last edited by Armynia; 12-28-2015, 06:47 AM.

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                • #48
                  Re: Military Aircrafts: Designs and Concepts

                  U.S. McDonnell Douglas F-4 Phantom II









                  General characteristics

                  Crew: 2
                  Length: 63 ft 0 in (19.2 m)
                  Wingspan: 38 ft 4.5 in (11.7 m)
                  Height: 16 ft 6 in (5.0 m)
                  Wing area: 530.0 ft² (49.2 m²)
                  Airfoil: NACA 0006.4–64 root, NACA 0003-64 tip
                  Empty weight: 30,328 lb (13,757 kg)
                  Loaded weight: 41,500 lb (18,825 kg)
                  Max. takeoff weight: 61,795 lb (28,030 kg)
                  Powerplant: 2 × General Electric J79-GE-17A axial compressor turbojets, 11,905 lbf dry thrust (52.9 kN), 17,845 lbf in afterburner (79.4 kN) each
                  Zero-lift drag coefficient: 0.0224
                  Drag area: 11.87 ft² (1.10 m²)
                  Aspect ratio: 2.77
                  Fuel capacity: 1,994 U.S. gal (7,549 L) internal, 3,335 U.S. gal (12,627 L) with three external tanks (370 U.S. gal (1,420 L) tanks on the outer wing hardpoints and either a 600 or 610 U.S. gal (2,310 or 2,345 L) tank for the centerline station).
                  Maximum landing weight: 36,831 lb (16,706 kg)


                  Performance

                  Maximum speed: Mach 2.23 (1,472 mph, 2,370 km/h) at 40,000 ft (12,190 m)
                  Cruise speed: 506 kn (585 mph, 940 km/h)
                  Combat radius: 367 nmi (422 mi, 680 km)
                  Ferry range: 1,403 nmi (1,615 mi, 2,600 km) with 3 external fuel tanks
                  Service ceiling: 60,000 ft (18,300 m)
                  Rate of climb: 41,300 ft/min (210 m/s)
                  Wing loading: 78 lb/ft² (383 kg/m²)
                  lift-to-drag: 8.58
                  Thrust/weight: 0.86 at loaded weight, 0.58 at MTOW
                  https://en.wikipedia.org/wiki/McDonn...F-4_Phantom_II

                  Comment

                  • #49
                    Re: Military Aircrafts: Designs and Concepts

                    U.S. McDonnell Douglas F-15C Eagle









                    General characteristics

                    Crew: 1: pilot
                    Length: 63 ft 9 in (19.43 m)
                    Wingspan: 42 ft 10 in (13.05 m)
                    Height: 18 ft 6 in (5.63 m)
                    Wing area: 608 ft² (56.5 m²)
                    Airfoil: NACA 64A006.6 root, NACA 64A203 tip
                    Empty weight: 28,000 lb (12,700 kg)
                    Loaded weight: 44,500 lb (20,200 kg)
                    Max. takeoff weight: 68,000 lb (30,845 kg)
                    Powerplant: 2 × Pratt & Whitney F100-100 or −220 afterburning turbofans
                    Dry thrust: 14,590 lbf[124] (64.9 kN) each
                    Thrust with afterburner: 23,770 lbf for −220 (105.7 kN for −220) each
                    Fuel capacity: 13,455 lb (6,100 kg) internal


                    Performance

                    Maximum speed:
                    High altitude: Mach 2.5+ (1,650+ mph, 2,665+ km/h)
                    Low altitude: Mach 1.2 (900 mph, 1,450 km/h)
                    Combat radius: 1,061 nmi (1,222 mi, 1,967 km) for interdiction mission
                    Ferry range: 3,450 mi (3,000 nmi, 5,550 km) with conformal fuel tanks and three external fuel tanks
                    Service ceiling: 65,000 ft (20,000 m)
                    Rate of climb: >50,000 ft/min (254 m/s)
                    Wing loading: 73.1 lb/ft² (358 kg/m²)
                    Thrust/weight: 1.07 (−220)
                    Maximum design g-load: 9 g
                    https://en.wikipedia.org/wiki/McDonn...las_F-15_Eagle

                    Comment

                    • #50
                      Re: Military Aircrafts: Designs and Concepts

                      U.S. McDonnell Douglas F/A-18 Hornet








                      General characteristics

                      Crew: F/A-18C: 1, F/A-18D: 2 (pilot and weapons system officer)
                      Length: 56 ft (17.1 m)
                      Wingspan: 40 ft (12.3 m)
                      Height: 15 ft 4 in (4.7 m)
                      Wing area: 400 ft² (38 m²)
                      Airfoil: NACA 65A005 mod root, 65A003.5 mod tip
                      Empty weight: 23,000 lb (10,400 kg)
                      Loaded weight: 36,970 lb (16,770 kg)
                      Max. takeoff weight: 51,900 lb (23,500 kg)
                      Powerplant: 2 × General Electric F404-GE-402 turbofans
                      Dry thrust: 11,000 lbf (48.9 kN) each
                      Thrust with afterburner: 17,750 lbf (79.2 kN) each
                      Fuel capacity: 10,860 pounds (4,930 kg) internally


                      Performance

                      Maximum speed:
                      High altitude: Mach 1.8 (1,034 knots, 1,190 mph, 1,915 km/h) at 40,000 ft (12,190 m)
                      Low altitude: Mach 1.2 (795 knots, 915 mph, 1,473 km/h)[129]
                      Range: 1,089 nmi (1,250 miles, 2,000 km) with only two AIM-9s
                      Combat radius: 400 nmi (460 mi (740 km)) on air-air mission
                      Ferry range: 1,800 nmi (2,070 mi (3,330 km))
                      Service ceiling: 50,000 ft (15,240 m)
                      Rate of climb: 50,000 ft/min (254 m/s)
                      Wing loading: 93 lb/ft² (454 kg/m²)
                      Thrust/weight: 0.96 (1.13 with loaded weight & 50% internal fuel)
                      https://en.wikipedia.org/wiki/McDonn..._F/A-18_Hornet

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