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CC-130J Super Hercules

CC-130J Super Hercules

Military Transport Aircrafts
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Basic Information
Name
CC-130J Super Hercules
Designation
CC-130J Super Hercules
Alternate Designation
C-130J-30, Hercules II, Shimshon (Israeli Air Force)
Equipment Type
Military Transport Aircrafts
Manufacturer
Lockheed Martin
Date of Introduction
1999
Description

The CC-130J, formerly known as the C-130J-30, is a stretch version, adding 15 feet to fuselage, increasing usable space in the cargo compartment, which translates to 30 percent more usable volume for increased seating, litters, pallets or airdrop platforms. This bigger cargo compartment can accommodate up to 7 pallets, 2 more than C-130J, and up to 92 paratroopers or 128 troops and their equipment, 28 more than C-130J. The long fuselage Super Hercules features a strengthened cargo ramp and improved airdrop system, allowing crews to make airdrops at 250 knots, which helps them avoid antiaircraft fire in hostile areas. The US Air Force cleared the container delivery system on the CC-130J aircraft in February 2005. In July 2004, the Royal Danish Air Force notified Lockheed-Martin that it will exercise an option for one C-130J Super Hercules (long-fuselage version) in addition to three already delivered C-130Js ordered in December 2000. The contract for one additional C-130J was signed in October 2004. Lockheed-Martin delivered the last of 22 C-130Js, a CC-130J, ordered by the Italian Air Force on 10 February 2005. Super Hercules deliveries to Italy began in 2000 with first order for 18 aircraft placed in 1997, two more in 1999 and two more in 2000 completing 12 C-130Js and 10 CC-130Js. As of 2005, these aircraft had been involved in tactical transport missions in Iraq and Afghanistan with the Italian Air Force.

Air & Air Defense Specifications
Crew 3
Max Speed 694.8 km/h
Range 4661.0 km
Service Ceiling 10058 m
Wingspan 39.70 m
Overview (Deagel)
Group Military Transport Aircrafts
Status Active
Also Known As C-130J-30, Hercules II, Shimshon (Israeli Air Force)
Origin United States of America
Contractor Lockheed Martin
Initial Operational Capability (IOC) 1999
Total Production 215
Unitary Cost USD $330 million
Specifications (Deagel)
Crew 3
Number of Engines 4
Troops 92
Dimensions — Height 11.4 meter
Dimensions — Length 34.7 meter
Dimensions — Wingspan 39.7 meter
Mass — Cargo 21,234 kilogram
Mass — Max Takeoff Weight 74,390 kilogram
Performance — Ceiling 10,058 meter
Performance — Max Range 4,661 kilometer
Power — Max Power at TakeOff 18,364 shp
Speed — Top Speed at High Altitude 193 mps
Gear (Deagel)
Item 1 Communications Devices: AN/ARC-210
Item 2 Communications Devices: AN/ARC-222
Item 3 Decoy Systems: AN/ALE-47
Item 4 ESM & Warning Systems: AN/AAR-47
Item 5 ESM & Warning Systems: AN/AAR-60 MILDS
Item 6 ESM & Warning Systems: AN/ALR-56
Item 7 Jamming Systems: AN/ALQ-211 SIRFC
Item 8 Jamming Systems: ELT/572
Item 9 Optronic Systems: Star SAFIRE
Item 10 Radar Systems: AN/APN-241 (1)
Item 11 Turboprop Engines: AE 2100D3 (4)
Variants
Variant 1 C-130H Hercules
Variant 2 MC-130H Talon II
Variant 3 AC-130U Spooky
Variant 4 C-130J Super Hercules
Variant 5 CC-130J Super Hercules
Variant 6 KC-130J Super Hercules
Variant 7 WC-130J
Variant 8 MC-130W Combat Spear
Variant 9 EC-130J Commando Solo
Variant 10 MC-130J Commando II
Variant 11 AC-130J Ghostrider
Variant 12 LM-100J
Variant 13 C-130J-SOF
Details
Country of Origin United States
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
34.7 m
Width
39.7 m
Height
11.4 m
Weight
74390 kg
Operators (22)
United States
France
United Kingdom
Israel
Italy
South Korea
India
Algeria
Australia
Canada
Denmark
Egypt
Indonesia
Iraq
Mexico
New Zealand
Norway
Oman
Philippines
Qatar
Tunisia
United Arab Emirates
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