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MH-47G Chinook

MH-47G Chinook

Utility & Transport Helicopters
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Basic Information
Name
MH-47G Chinook
Designation
MH-47G Chinook
Alternate Designation
Equipment Type
Utility & Transport Helicopters
Manufacturer
Boeing
Date of Introduction
2004
Description

The MH-47G will be a derivative of improved CH-47F helicopter. The MH-47G aircraft will fulfill the US Army special operations requirements in the 21st century. The US Army current plans call for procurement of 37 new-build MH-47Gs and remanufacture of 58 existing C/MH-47E/D helicopters to the G-model standard by 2011. Boeing delivered the first MH-47G Special Operations Chinook aircraft to the US Army on May 7, 2004. In September 2005, Boeing unveiled its proposal designated as the HH-47 CSAR-X for the US Air Force Combat Search and Rescue program. The HH-47 CSAR-X powered by T-55-GA-714A engines was based upon MH-47G airframe, countermeasures and survivability systems. As of January 2005, the latest US Army's acquisition plan approved the increase of the Chinook fleet from 463 to 513 aircraft. The plan included upgrade of the entire fleet of 397 CH-47Ds to the F-model configuration and acquisition of at least 55 additional new-build CH-47Fs. The US Special Operations Command will increase their current fleet of 34 MH-47D/E special operations heavy assault Chinooks to 61 MH-47Gs, with options on further aircraft. On January 14, 2005, Boeing was awarded a $194 million contract as part of a $223 million fixed-price-incentive contract to remanufacture 12 CH-47 helicopters to the MH-47G configuration. Modification work is expected to conclude by July 30, 2006.

Air & Air Defense Specifications
Crew 2
Max Speed 315.0 km/h
Range 1136.0 km
Service Ceiling 3094 m
Overview (Deagel)
Group Utility & Transport Helicopters
Status Active
Origin United States of America
Contractor Boeing
Initial Operational Capability (IOC) May 7, 2004
Total Production 37
Specifications (Deagel)
Crew 2
Main Rotor Blades 6
Number of Engines 2
Troops 44
Dimensions — Height 5.5 meter
Dimensions — Length 30.2 meter
Dimensions — Main Rotor Diameter 18.3 meter
Dimensions — Width 3.6 meter
Mass — Empty Weight 12,210 kilogram
Mass — Max Takeoff Weight 24,945 kilogram
Mass — Payload 12,285 kilogram
Performance — Ceiling 3,094 meter
Performance — Max Range 1,136 kilometer
Power — Max Power at TakeOff 7,258 shp
Speed — Cruise Speed 259 kph
Speed — Top Speed at High Altitude 315 kph
Time — Flight Endurance 5.5 hour
Gear (Deagel)
Item 1 Optronic Systems: AN/AAQ-16 (1)
Item 2 Radar Systems: AN/APQ-174 (1)
Item 3 Radar Systems: Silent Knight (1)
Item 4 Tactical Vehicles: LSV (1)
Item 5 Turboshaft Engines: T-55-GA-714A (2)
Variants
Variant 1 CH-47D Chinook
Variant 2 MH-47E Chinook
Variant 3 MH-47G Chinook
Variant 4 CH-47F Chinook
Variant 5 HH-47 Chinook
Variant 6 MH-47G Block II Chinook
Variant 7 CH-47F Block II Chinook
Details
Country of Origin United States
Category Transport Helicopter
Air > Transport Helicopter
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
30.2 m
Width
Height
5.5 m
Weight
24945 kg
Related Equipment (1)
Operators (1)
United States
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