Military Aircrafts: Designs and Concepts

[Artashes]

Re: Military Aircrafts: Designs and Concepts

I'm not computer savvy enough to post pics/info.
I'd like to see the Yak 130 trainor / light attack aircraft posted in this format.
My #1 choice for trainor/general duty plane.

[Armynia]

Re: Military Aircrafts: Designs and Concepts

U.S. Mcdonnell Douglas F/A-18E/F Super Hornet

General characteristics

Crew: F/A-18E: 1, F/A-18F: 2
Length: 60 ft 1¼ in (18.31 m)
Wingspan: 44 ft 8½ in (13.62 m)
Height: 16 ft (4.88 m)
Wing area: 500 ft² (46.5 m²)
Empty weight: 32,081 lb (14,552 kg)
Loaded weight: 47,000 lb (21,320 kg) (in fighter configuration))
Max. takeoff weight: 66,000 lb (29,937 kg)
Powerplant: 2 × General Electric F414-GE-400 turbofans
Dry thrust: 13,000 lbf (62.3 kN) each
Thrust with afterburner: 22,000 lbf (97.9 kN) each
Internal fuel capacity: F/A-18E: 14,400 lb (6,780 kg), F/A-18F: 13,550 lb (6,354 kg)
External fuel capacity: 5 × 480 gal tanks, totaling 16,380 lb (7,381 kg)


Performance

Maximum speed: Mach 1.8 (1,190 mph, 1,915 km/h) at 40,000 ft (12,190 m)
Range: 1,275 nmi (2,346 km) clean plus two AIM-9s[14]
Combat radius: 390 nmi (449 mi, 722 km) for interdiction mission[152]
Ferry range: 1,800 nmi (2,070 mi, 3,330 km)
Service ceiling: 50,000+ ft (15,000+ m)
Rate of climb: 44,882 ft/min[153] (228 m/s)
Wing loading: 94.0 lb/ft² (459 kg/m²)
Thrust/weight: 0.93
Design load factor: 7.6 g
https://en.wikipedia.org/wiki/Boeing...F_Super_Hornet




For More General Military Aircrafts List....http://forum.hyeclub.com/showthread....s-and-Concepts

[Armynia]

Re: Military Aircrafts: Designs and Concepts

Japan, Mitsubishi F-1











General characteristics

Crew: 1
Length: 17.86 m (58 ft 7 in)
Wingspan: 7.88 m (25 ft 10¼ in)
Height: 4.48 m (14 ft 8⅓ in)
Wing area: 21.2 m² (228 ft²)
Empty weight: 6,358 kg (14,017 lb)
Max. takeoff weight: 13,674 kg (30,146 lb)
Powerplant: 2 × Ishikawa-Harima TF40-801A turbofan
Dry thrust: 22.8 kN (5,115 lbf) each
Thrust with afterburner: 35.6 kN (7,305 lbf) each


Performance

Maximum speed: 1,700 km/h (918 knots, 1,056 mph) at 11,000 m (36,100 ft) (clean)
Combat radius: 556 km (483 nmi, 346 mi) High-Low-High profile with two ASM-1 missiles and one 830 L (183 Imp gallon) drop tank
Ferry range: 2,870 km (1,552 nmi, 1,785 mi) (max external fuel)
Service ceiling: 15,240 m[7] (50,000 ft)
Rate of climb: 118 m/s (35,000 ft/min)
Wing loading: 645 kg/m² (132 lb/ft²)
Climb to 11,000 m (36,100 ft): 2.0 min
https://en.wikipedia.org/wiki/Mitsubishi_F-1




For More General Military Aircrafts List....http://forum.hyeclub.com/showthread....s-and-Concepts

[Armynia]

Re: Military Aircrafts: Designs and Concepts

U.S. North American F-86 Sabre











General characteristics

Crew: 1
Length: 37 ft 1 in (11.4 m)
Wingspan: 37 ft 0 in (11.3 m)
Height: 14 ft 1 in (4.5 m)
Wing area: 313.4 sq ft (29.11 m²)
Empty weight: 11,125 lb (5,046 kg)
Loaded weight: 15,198 lb (6,894 kg)
Max. takeoff weight: 18,152 lb (8,234 kg)
Powerplant: 1 × General Electric J47-GE-27 turbojet, 5,910 lbf (26.3 kN)
Fuel provisions Internal fuel load: 437 US gallons (1,650 L), Drop tanks: 2x200 US gallons (760 L) JP-4 fuel


Performance

Maximum speed: 687 mph (1,106 km/h) at sea level at 14,212 lb (6,447 kg) combat weight
also reported 678 mph (1,091 km/h) and 599 at 35,000 feet (11,000 m) at 15,352 pounds (6,960 kg). (597 knots (1,106 km/h) at 6446 m, 1,091 and 964 km/h at 6,960 m.)
Stall speed: 124 mph (power off) (108 knots (200 km/h))
Range: 1,525 mi, (2,454 km)
Service ceiling: 49,600 ft at combat weight (15,100 m)
Rate of climb: 9,000 ft/min at sea level (45.72 m/s)
Wing loading: 49.4 lb/ft² (236.7 kg/m²)
lift-to-drag: 15.1
Thrust/weight: 0.42
https://en.wikipedia.org/wiki/North_American_F-86_Sabre

[Armynia]

Re: Military Aircrafts: Designs and Concepts

U.S. North American YF-93








General characteristics

Crew: One
Length: 44 ft 1 in (13.44 m)
Wingspan: 38 ft 9 in (11.81 m)
Height: 15 ft 8 in (4.78 m)
Wing area: 306 ft² (28.4 m²)
Empty weight: 14,035 lb (6,366 kg)
Loaded weight: 21,610 lb (9,800 kg)
Powerplant: 1 × Pratt & Whitney J48-P-6 turbojet, 8,750 lbf (38.9 kN)


Performance

Maximum speed: 708 mph (1,132 km/h)
Range: 2,000 mi (3,200 km)
Service ceiling: 46,800 ft (14,268 m)
Rate of climb: 11,960 ft/min (60.8 m/s)
Wing loading: 71 lb/ft² (345 kg/m²)
Thrust/weight: 0.4
https://en.wikipedia.org/wiki/North_American_YF-93

[Armynia]

Re: Military Aircrafts: Designs and Concepts

U.S. North American F-100 Super Sabre










General characteristics

Crew: 1
Length: 50 ft (15.2 m)
Wingspan: 38 ft 9 in (11.81 m)
Height: 16 ft 2¾ in (4.95 m)
Wing area: 400 ft² (37 m²)
Empty weight: 21,000 lb (9,500 kg)
Loaded weight: 28,847 lb (13,085 kg)
Max. takeoff weight: 34,832 lb (15,800 kg)
Powerplant: 1 × Pratt & Whitney J57-P-21/21A turbojet
Dry thrust: 10,200 lbf (45 kN)
Thrust with afterburner: 16,000 lbf (71 kN)
*Zero-lift drag coefficient: 0.0130
Drag area: 5.0 ft² (0.46 m²)
Aspect ratio: 3.76


Performance

Maximum speed: 750 kn (864 mph, 1,390 km/h, Mach 1.3)
Range: 1,733 NM (1,995 mi, 3,210 km)
Service ceiling: 50,000 ft (15,000 m)
Rate of climb: 22,400 ft/min (114 m/s)
Wing loading: 72.1 lb/ft² (352 kg/m²)
Thrust/weight: 0.55
Lift-to-drag ratio: 13.9
https://en.wikipedia.org/wiki/North_...00_Super_Sabre

[Armynia]

Re: Military Aircrafts: Designs and Concepts

U.S. Northrop F-5 Freedom Fighter

General characteristics

Crew: 1
Length: 47 ft 4¾ in (14.45 m)
Wingspan: 26 ft 8 in (8.13 m)
Height: 13 ft 4½ in (4.08 m)
Wing area: 186 ft² (17.28 m²)
Airfoil: NACA 65A004.8 root, NACA 64A004.8 tip
Empty weight: 9,558 lb (4,349 kg)
Loaded weight: 15,745 lb (7,157 kg)
Max. takeoff weight: 24,722 lb (11,214 kg)
Powerplant: 2 × General Electric J85-GE-21B turbojet
Dry thrust: 3,500 lbf (15.5 kN) each
Thrust with afterburner: 5,000 lbf (22.2 kN) each
Zero-lift drag coefficient: 0.0200
Drag area: 3.4 ft² (0.32 m²)
Aspect ratio: 3.82
Internal fuel: 677 U.S. gal (2,563 L)
External fuel: 275 U.S. gal (1,040 L) per tank in up to 3 tanks


Performance

Maximum speed: 917 kn (Mach 1.6, 1,060 mph, 1,700 km/h) ; at altitude
Range: 760 nmi (870 mi, 1,405 km)
Ferry range: 2,010 nmi (2,310 mi, 3,700 km[153])
Service ceiling: 51,800 ft (15,800 m)
Rate of climb: 34,400 ft/min (175 m/s)
Lift-to-drag ratio: 10.0
https://en.wikipedia.org/wiki/Northrop_F-5

[Armynia]

Re: Military Aircrafts: Designs and Concepts

U.S. U.K. Italy and West Germany, Panavia Tornado













General characteristics

Crew: 2
Length: 16.72 m (54 ft 10 in)
Wingspan: 13.91 m at 25° wing sweep, 8.60 m at 67° wing sweep (45.6 ft / 28.2 ft)
Height: 5.95 m (19.5 ft)
Wing area: 26.6 m2 (286 ft2)
Empty weight: 13,890 kg (30,620 lb)
Loaded weight: 20,240 kg (44,620 lb)
Max. takeoff weight: 28,000 kg (61,700 lb)
Powerplant: 2 × Turbo-Union RB199-34R Mk 103 afterburning turbofans
Dry thrust: 43.8 kN (9,850 lbf) each
Thrust with afterburner: 76.8 kN (17,270 lbf) each


Performance

Maximum speed: Mach 2.2 (2,400 km/h, 1,490 mph) at 9,000 m (30,000 ft) altitude; 800 knots, 1,482 km/h, 921 mph indicated airspeed near sea level
Range: 1,390 km (870 mi) typical combat
Ferry range: 3,890 km (2,417 mi) with four external drop tanks
Service ceiling: 15,240 m (50,000 ft)
Rate of climb: 76.7 m/s (15,100 ft/min)
Thrust/weight: 0.77
https://en.wikipedia.org/wiki/Panavia_Tornado

[Armynia]

Re: Military Aircrafts: Designs and Concepts

U.S. Republic F-84 Thunderjet

General characteristics

Crew: one
Length: 38 ft 1 in (11.60 m)
Wingspan: 36 ft 5 in (11.10 m)
Height: 12 ft 7 in (3.84 m)
Wing area: 260 ft² (24 m²)
Empty weight: 11,470 lb (5,200 kg)
Loaded weight: 18,080 lb (8,200 kg)
Max. takeoff weight: 23,340 lb (10,590 kg)
Powerplant: 1 × Allison J35-A-29 turbojet, 5,560 lbf (24.7 kN)


Performance

Maximum speed: 622 mph (540 kn, 1,000 km/h,Mach .81)
Cruise speed: 475 mph (413 kn, 770 km/h)
Range: 1,000 mi (870 nmi, 1,600 km) combat
Ferry range: 2,000 mi (1,700 nmi, 3,200 km) with external tanks
Service ceiling: 40,500 ft (12,350 m)
Rate of climb: 3,765 ft/min (19.1 m/s)
Wing loading: 70 lb/ft² (342 kg/m²)
Thrust/weight: 0.31 lbf/lb
https://en.wikipedia.org/wiki/Republic_F-84_Thunderjet

[Armynia]

Re: Military Aircrafts: Designs and Concepts

Sweden, Saab J-29 Tunnan

General characteristics

Crew: 1
Length: 10.23 m (33 ft 7 in)
Wingspan: 11.0 m (36 ft 1 in)
Height: 3.75 m (12 ft 4 in)
Wing area: 24.15 m² (260.0 ft²)
Empty weight: 4,845 kg (10,680 lb)
Max. takeoff weight: 8,375 kg (18,465 lb)
Powerplant: 1 × Svenska Flygmotor RM 2B turbojet, 6,070 lbf (27 kN)


Performance

Maximum speed: 1,060 km/h (660 mph)
Range: 1,100 km (685 mi)
Service ceiling: 15,500 m (50,850 ft)
Rate of climb: 32.1 m/s (6,320 ft/min)