C-130H Hercules, CH-47F Chinook and UH-60L Blackhawk

Specifications C-130H Hercules

General characteristics
Crew: 5 (two pilots, navigator, flight engineer and loadmaster)
Capacity:

• C-130E/H/J cargo hold: length, 40 feet (12.31 meters); width, 119 inches (3.12 meters); height, 9 feet (2.74 meters). Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 meters)
• C-130J-30 cargo hold: length, 55 feet (16.9 meters); width, 119 inches (3.12 meters); height, 9 feet (2.74 meters). Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 meters)
• 92 passengers or
• 64 airborne troops or
• 74 litter patients with 2 medical personnel or
• 6 pallets or
• 2–3 Humvees or
• 2 M113 armored personnel carriers

Payload: 45,000 lb (20,000 kg)
Length: 97 ft 9 in (29.8 m)
Wingspan: 132 ft 7 in (40.4 m)
Height: 38 ft 3 in (11.6 m)
Wing area: 1,745 ft² (162.1 m²)
Empty weight: 75,800 lb (34,400 kg)
Useful load: 72,000 lb (33,000 kg)
Max. takeoff weight: 155,000 lb (70,300 kg)
Powerplant: 4 × Allison T56-A-15 turboprops, 4,590 shp (3,430 kW) each


Specifications CH-47F Chinook

General characteristics
Crew: 3 (pilot, copilot, flight engineer)
Capacity:
33–55 troops or
24 litters and 3 attendants or
28,000 lb (12,700 kg) cargo
Length: 98 ft 10 in (30.1 m)
Rotor diameter: 60 ft 0 in (18.3 m)
Height: 18 ft 11 in (5.7 m)
Disc area: 5,600 ft2 (2,800 ft2 per rotor disc) (260 m2)
Empty weight: 23,400 lb (10,185 kg)
Loaded weight: 26,680 lb (12,100 kg)
Max. takeoff weight: 50,000 lb (22,680 kg)
Powerplant: 2 × Lycoming T55-GA-714A turboshaft, 4,733 hp (3,631 kW) each


Specifications UH-60L Blackhawk


General characteristics
Crew: 2 pilots (flight crew) with 2 crew chiefs/gunners
Capacity: 2,640 lb (1,200 kg) of cargo internally, including 11 troops or 6 stretchers, or 8,000 lb (3,600 kg) (UH-60A) or 9,000 lb (4,100 kg) (UH-60L) of cargo externally
Length: 64 ft 10 in (19.76 m)
Fuselage width: 7 ft 9 in (2.36 m)
Rotor diameter: 53 ft 8 in (16.36 m)
Height: 16 ft 10 in (5.13 m)
Disc area: 2,260 ft² (210 m²)
Empty weight: 10,624 lb (4,819 kg)
Loaded weight: 22,000 lb (9,980 kg)
Max. takeoff weight: 23,500 lb (10,660 kg)
Powerplant: 2 × General Electric T700-GE-701C turboshaft, 1,890 hp (1,410 kW) each


Sumber :
http://www.the-blueprints.com/blueprints/modernplanes/lockheed/20067/view/lockheed_c-130_hercules/
http://www.helis.com/60s/CH-47_Chinook.php
http://www.inetres.com/gp/military/ar/rotor/UH-60A.html