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C-130J Super Hercules

C-130J Super Hercules

Military Transport Aircrafts
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Basic Information
Name
C-130J Super Hercules
Designation
C-130J Super Hercules
Alternate Designation
Hercules II, Super Hercules
Equipment Type
Military Transport Aircrafts
Manufacturer
Lockheed Martin
Date of Introduction
1999
Description

The C-130J Hercules II is the latest and most advanced derivative of the proven C-130 cargo aircraft and will replace ageing C-130Es aircraft. It incorporates state-of-the-art technology to reduce manpower requirements, operating, support, and life cycle costs over current C-130s. The J model also features improved maneuverability and handling, shorter runaways needs for taking off and landing than previous models. The new turboprops AE 2100D3 engines with 6 blades are one of the keys of the C-130J improved performance. The C-130J achieved initial operational capability in 1999. The US Air Force plans to purchase up to 168 C-130J and CC-130J (a stretch version of C-130J) aircraft to replace older C-130Es. The US Coast Guard operates the HC-130J model introduced into service in 2004. In December 2004, the US Air Force deployed the C-130J aircraft for the first time in support of air mobility operations around the world replacing earlier models. The C-130Js involved in such effort were from Rhode Island Air National Guard's 143rd Airlift Squadron, Maryland ANG's 135th AS, Air Force Reserve's Command's 815th AS at Keesler Air Force Base, Missouri, and California ANG's 115th AS at Channel Islands ANG Station. The Air Force was expected to procure up to 53 C-130Js valued at $6.2 billion as of June 2005. 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 705.6 km/h
Range 4390.0 km
Service Ceiling 10058 m
Wingspan 39.70 m
Overview (Deagel)
Group Military Transport Aircrafts
Status Active
Also Known As Hercules II, Super Hercules
Origin United States of America
Contractor Lockheed Martin
Initial Operational Capability (IOC) 1999
Total Production 72
Unitary Cost USD $73 million
Specifications (Deagel)
Crew 3
Number of Engines 4
Troops 64
Dimensions — Height 11.4 meter
Dimensions — Length 29.3 meter
Dimensions — Wingspan 39.7 meter
Mass — Cargo 21,151 kilogram
Mass — Max Takeoff Weight 70,308 kilogram
Performance — Ceiling 10,058 meter
Performance — Max Range 4,390 kilometer
Power — Max Power at TakeOff 18,364 shp
Speed — Top Speed at High Altitude 196 mps
Gear (Deagel)
Item 1 Decoy Systems: AN/ALE-55
Item 2 Decoy Systems: DASS-2000
Item 3 ESM & Warning Systems: AN/ALR-56M
Item 4 Jamming Systems: AAQ-24(V) LAIRCM
Item 5 Jamming Systems: ELT/572
Item 6 Radar Systems: AN/APN-241 (1)
Item 7 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
29.3 m
Width
39.7 m
Height
11.4 m
Weight
70308 kg
Operators (4)
United States
United Kingdom
Italy
Oman
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