Military Aircrafts: Designs and Concepts

[Armynia]

Re: Military Aircrafts: Designs and Concepts

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

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Re: Military Aircrafts: Designs and Concepts

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

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Re: Military Aircrafts: Designs and Concepts

U.K. Hawker Sea Hawk

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Re: Military Aircrafts: Designs and Concepts

U.S. Lockheed/Martin F-104 Starfighter

[Armynia]

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

[Armynia]

Re: Military Aircrafts: Designs and Concepts

Brazil, Embraer EMB 314 Super Tucano

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Re: Military Aircrafts: Designs and Concepts

U.S. McDonnell FH-1 Phantom

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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

[Armynia]

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

[Armynia]

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