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Lockheed Martin C-130J-30 Super Hercules

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Description

Second attempt to adding a real world aircraft in 6 profile drawing, still about the Big-J. 

This time the longer version.

Variants:

C-130J Super Hercules
Tactical airlifter

C-130J-30
Lockheed Martin designation for its 15 ft (4.6 m) extended fuselage variant.

CC-130J Super Hercules
Official USAF and Royal Canadian Air Force designation for the C-130J-30.

EC-130J Commando Solo III
Variant for the Air Force Special Operations Command, operated by the Pennsylvania Air National Guard.

HC-130J Combat King II
Long range patrol and air-sea rescue variant for the United States Coast Guard. USAF HC-130J version has changes for in-flight refueling.

KC-130J
Aerial refueling tanker and tactical airlifter version for United States Marine Corps.

MC-130J Commando II
Designed for Air Force Special Operations Command. Originally named Combat Shadow II.

WC-130J
Weather reconnaissance ("Hurricane Hunter") version for the Air Force Reserve Command.

Hercules C4
Royal Air Force designation for the C-130J-30

Hercules C5
Royal Air Force designation for the C-130J

L-100J
A civilian version of the C-130J-30 was under development, but the program was placed on hold indefinitely to focus on military development and production.

SC-130J-30 Sea Hercules 
Proposed maritime patrol version of the C-130J, designed for coastal surveillance and anti-submarine warfare.

General characteristics:

Crew: 3 (two pilots, and one loadmaster are minimum crew)

Capacity:
92 passengers (128 for C-130J-30) or
64 airborne troops (92 for C-130J-30) or
6 pallets (8 pallets for C-130J-30) or
74 litter patients with 2 medical personnel (97 litters for C-130J-30)
2–3 Humvees, or 1 LAV III (with turret removed) or an M113 armored personnel carrier

Payload: 42,000 lb (19,050 kg) ; for C-130J-30: 44,000 lb/ 19,958 kg
Length: 97 ft 9 in, 29.79 m (for C-130J-30: 112 ft, 9 in, 34.36 m)
Wingspan: 132 ft 7 in (40.41 m)
Height: 38 ft 10 in (11.84 m)
Wing area: 1,745 ft² (162.1 m²)
Empty weight: 75,562 lb (34,274 kg)
Useful load: 72,000 lb (33,000 kg)
Max. takeoff weight: up to 175,000 lb (79,378 kg); normal 155,000 lb (70,305 kg)

Powerplant: 4 × Rolls-Royce AE 2100D3 turboprop, 4,637 shp (3,458 kW) each
Propellers: Dowty R391 6-blade composite propeller, 1 per engine
Performance
Maximum speed: 362 knots (417 mph, 671 km/h)
Cruise speed: 348 knots (400 mph, 643 km/h)
Range: 2,835 nmi (3,262 mi, 5,250 km)
Service ceiling: 28,000 ft (8,615 m) with 42,000 pounds (19,090 kilograms) payload
Absolute altitude 40,386 ft (12,310 m)[101]
Takeoff distance: 3,127 ft (953 m) at 155,000 lb (70,300 kg) gross weight

Lockheed Martin logo was courtesy of bagera3005 
Image size
3508x2631px 2.17 MB
Comments8
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Is there anyway you could make a Yokota version of this?