CH-47 Chinook: Difference between revisions
imported>Howard C. Berkowitz No edit summary |
mNo edit summary |
||
| (9 intermediate revisions by 3 users not shown) | |||
| Line 1: | Line 1: | ||
{{subpages}} | {{subpages}} | ||
{{TOC|right}} | {{TOC|right}} | ||
[[Image:CH-47.JPG|thumb|CH-47 helicopters in Hurricane Rita relief]] | [[Image:CH-47.JPG|thumb|350px|right|CH-47 helicopters in Hurricane Rita relief]] | ||
The '''H-47''' or '''CH-47 Chinook''' is the current U.S. Army medium lift helicopters, with a distinctive tandem-rotor configuration, is operated by 16 nations. The '''MH-47 Chinook''' is a special operations variant. | The '''H-47''' or '''CH-47 Chinook''' is the current U.S. Army medium lift helicopters, with a distinctive tandem-rotor configuration, is operated by 16 nations. The '''MH-47 Chinook''' is a special operations variant. | ||
| Line 25: | Line 25: | ||
===CH-47C=== | ===CH-47C=== | ||
First built in 1967, the C model improved performance, with a external load capacity of 20,000 pounds. Again, the engine was upgraded and the structure strengthened. There were also safety improvements, but the B and C models were incremental improvements to the original aircraft. | First built in 1967, the C model improved performance, with a external load capacity of 20,000 pounds. Again, the engine was upgraded and the structure strengthened. There were also safety improvements, but the B and C models were incremental improvements to the original aircraft. | ||
[[Image:Ch-47 carrying how+trk.jpg|left|thumb|Externally carried load]] | [[Image:Ch-47 carrying how+trk.jpg|left|thumb|350px|Externally carried load]] | ||
===CH-47D=== | ===CH-47D=== | ||
D models resulted from a 1976 contract to modernize the series. The contract started by stripping A, B and C models to the basic airframe, and rebuilding into prototypes. Again, there was an engine upgrade, as well as incremental improvements in the cooling and rotors. | D models resulted from a 1976 contract to modernize the series. The contract started by stripping A, B and C models to the basic airframe, and rebuilding into prototypes. Again, there was an engine upgrade, as well as incremental improvements in the cooling and rotors. | ||
| Line 35: | Line 35: | ||
Load capacity is twice that of an A model. Representative internal loads include 33 to 44 troops, or 24 litters plus two medical attendants. It can carry up to 26,000 pounds externally. The CH-47D has three cargo hooks: a center (main) hook and two additional hooks fore and aft of the main hook. | Load capacity is twice that of an A model. Representative internal loads include 33 to 44 troops, or 24 litters plus two medical attendants. It can carry up to 26,000 pounds externally. The CH-47D has three cargo hooks: a center (main) hook and two additional hooks fore and aft of the main hook. | ||
The [[Gulf War#Preparation for the "Left Hook" |"left hook"]] of the [[Gulf War]] was paced by the operational radius of a D model, which was the workhorse of forward transportation. | The [[Gulf War (Iraq, 1991)#Preparation for the "Left Hook" |"left hook"]] of the [[Gulf War (Iraq, 1991)|Gulf War]] was paced by the operational radius of a D model, which was the workhorse of forward transportation. | ||
===Improved Cargo Helicopter (ICH)/F model=== | ===Improved Cargo Helicopter (ICH)/F model=== | ||
| Line 43: | Line 43: | ||
| author = Boeing Company}}</ref> | | author = Boeing Company}}</ref> | ||
Improvements for situational awareness center around the [[MIL-STD-1553]] bus, including an advanced digital map display and a data transfer system that allows storing of preflight and mission data. Improved survivability features include the [[AAR-57|AN/AAR-57]] Common Missile Warning and | Improvements for situational awareness center around the [[MIL-STD-1553]] bus, including an advanced digital map display and a data transfer system that allows storing of preflight and mission data. Improved survivability features include the [[AAR-57|AN/AAR-57]] Common Missile Warning and ALE-47 Improved Countermeasure Dispenser Systems. | ||
Airframe structural modifications will reduce harmful vibrations, reducing operations and support (O&S) costs and improving crew endurance. Other airframe modifications will reduce by approximately 60% the time required for aircraft tear down and build-up after deployment on a C-5 or C-17. These modifications will significantly enhance the Chinook’s strategic deployment capability. <ref name=Armyfact-CH47>{{citation | Airframe structural modifications will reduce harmful vibrations, reducing operations and support (O&S) costs and improving crew endurance. Other airframe modifications will reduce by approximately 60% the time required for aircraft tear down and build-up after deployment on a C-5 or C-17. These modifications will significantly enhance the Chinook’s strategic deployment capability. <ref name=Armyfact-CH47>{{citation | ||
| Line 54: | Line 54: | ||
MH-47C/D/E Special Operations Aircraft (SOA) is a derivative of the Boeing CH-47 Chinook, with extensive modifications to the fuel system, including greater capacity, air refueling (D and E only) and survivability improvements such as inert gas fillers for the fuel tanks. Eventually, all will be E models until remanufacture into the MH-60G. | MH-47C/D/E Special Operations Aircraft (SOA) is a derivative of the Boeing CH-47 Chinook, with extensive modifications to the fuel system, including greater capacity, air refueling (D and E only) and survivability improvements such as inert gas fillers for the fuel tanks. Eventually, all will be E models until remanufacture into the MH-60G. | ||
The avionics have been enhanced for all-weather and night operations. Having a larger special operations helicopter gives | The avionics have been enhanced for all-weather and night operations. Having a larger special operations helicopter gives U.S. Special Operations Command the ability to do behind-the-lines deliveries of vehicle-borne teams. | ||
==Current operations== | ==Current operations== | ||
While several Chinooks sank with the cargo ship ''Atlantic Conveyor'', the Chinook was essential to the U.K. operations in the [[Falklands War]]. | While several Chinooks sank with the cargo ship ''Atlantic Conveyor'', the Chinook was essential to the U.K. operations in the [[Falklands War]]. | ||
The amount of load a cargo helicopter can carry depends on the model, the fuel on board, the distance to be flown, and atmospheric conditions.<ref name=FAS-CH47 /> In the high mountains of | The amount of load a cargo helicopter can carry depends on the model, the fuel on board, the distance to be flown, and atmospheric conditions.<ref name=FAS-CH47 /> In the high mountains of Afghanistan, these helicopters have done surprisingly well, while lighter helicopters' engines struggle. | ||
CH-47's are in the | CH-47's are in the Aviation Brigade of the new U.S. Army restructuring into brigades. | ||
==General characteristics== | ==General characteristics== | ||
| Line 75: | Line 75: | ||
* Minimum Crew: 3 (pilot, co-pilot, and flight engineer) | * Minimum Crew: 3 (pilot, co-pilot, and flight engineer) | ||
==References== | ==References== | ||
{{reflist}} | {{reflist}}[[Category:Suggestion Bot Tag]] | ||
Latest revision as of 16:00, 22 July 2024
The H-47 or CH-47 Chinook is the current U.S. Army medium lift helicopters, with a distinctive tandem-rotor configuration, is operated by 16 nations. The MH-47 Chinook is a special operations variant.
These helicopters can carry troops, cargo, and small vehicles internally, and larger loads, such as a howitzer, hung from a sling that attaches to the bottom of the helicopter.
History
Development of the medium lift Boeing Vertol (models 114 and 414) CH-47 Series Chinook began in 1956.[1]
In the Tactical Mobility Requirements Board analysis of the potential of helicopter-borne air assault, the ability of the Chinook to move light vehicles and artillery was essential to the success of the AIR ASSAULT II test.
Versions
The series is turning into a very long-lived family, like the C-130 Hercules or B-52. Besides the improvements in each new developmental version, there has been a good deal of remanufacturing.
CH-47A
The winner of a 1958 Army solicitation for a medium transport helicopter, the CH-47A preceded the deployment of air assault units in the Vietnam War. A-models were first used there in 1962, but had a critical role in the Howze Board AIR ASSAULT II feasibility demonstration of an airmobile division.
Early production CH-47A’s operated with the 11th Air Assault Division during 1963 and in October of that year the aircraft was formally designated as the Army’s standard medium transport helicopter. In June 1965 the 11th Air Assault Division was redesignated as the 1st Cavalry Division (Airmobile) and readied for deployment to Viet Nam. Chinooks from the 11th Air Assault formed the nucleus of the 228th Assault Helicopter Battalion which began operations in Viet Nam in September, 1965. CH-47A’s deployed to Viet Nam were equipped with Lycoming T55-L7 engines generating 2650 shp. The aircraft had a maximum gross weight of 33,000 pounds allowing for a maximum payload of approximately 10,000 pounds. The hot mountainous conditions of Viet Nam limited the A models performance capabilities and generated a requirement for increased payload and better performance.
CH-47B
In the environmental conditions of Viet Nam, the A model was underpowered. The B model was an interim upgrade, with a more powerful engine and more rugged airframe, with rotor and fuselage aerodynamic changes that improved stability.
CH-47C
First built in 1967, the C model improved performance, with a external load capacity of 20,000 pounds. Again, the engine was upgraded and the structure strengthened. There were also safety improvements, but the B and C models were incremental improvements to the original aircraft.
CH-47D
D models resulted from a 1976 contract to modernize the series. The contract started by stripping A, B and C models to the basic airframe, and rebuilding into prototypes. Again, there was an engine upgrade, as well as incremental improvements in the cooling and rotors.
New features, however, included a redesigned cockpit to reduce pilot workload, redundant and improved electrical systems, modularized hydraulic systems, an advanced flight control system, and improved avionics. The D model can be refueled in flight.
As an armed helicopter, it an be equipped with two door mounting M60D 7.62mm machine guns on the M24 armament subsystem and a ramp mounting M60D using the M41 armament subsystem.
Load capacity is twice that of an A model. Representative internal loads include 33 to 44 troops, or 24 litters plus two medical attendants. It can carry up to 26,000 pounds externally. The CH-47D has three cargo hooks: a center (main) hook and two additional hooks fore and aft of the main hook.
The "left hook" of the Gulf War was paced by the operational radius of a D model, which was the workhorse of forward transportation.
Improved Cargo Helicopter (ICH)/F model
Yet another remanufacturing process upgrade the D model's engine, and rebuilt the airframe to have another 20 years of service, putting the aircraft into the honored few that will be in service past the half-century mark. Both crew and avionics will be happier due to vibration reduction, and the MIL-STD-1533 bus is added to enable integration with a wide range of nondevelopmental avionics, including Force XXI Army digital architecture. Its avionics include a Rockwell Collins Common Avionics Architecture System (CAAS) cockpit and a BAE Digital Advanced Flight Control System (DAFCS). DAFCS provides dramatically improved flight control capabilities through features such as "hover hold," "altitude hold" and "beep down" that improve performance and safety in brownout situations as well as the entire flight envelope. [2]
Improvements for situational awareness center around the MIL-STD-1553 bus, including an advanced digital map display and a data transfer system that allows storing of preflight and mission data. Improved survivability features include the AN/AAR-57 Common Missile Warning and ALE-47 Improved Countermeasure Dispenser Systems.
Airframe structural modifications will reduce harmful vibrations, reducing operations and support (O&S) costs and improving crew endurance. Other airframe modifications will reduce by approximately 60% the time required for aircraft tear down and build-up after deployment on a C-5 or C-17. These modifications will significantly enhance the Chinook’s strategic deployment capability. [3]
Fatcow
With a less than dignified name but an essential function, the Fatcow is a CH-47 with the Extended Range Fuel System [ERFS] II system located in the cargo bay. The configuration consists of three or four fuel tanks attached to a refueling system. The system contains 2400 gallons of JP4/8 excluding the CH-47 internal fuel load of 1050 gals. The Fatcow can set up a 1,2,3,or 4 point system using Hot Tactical Aircraft Refueling System (HTARS}.
MH-47
MH-47C/D/E Special Operations Aircraft (SOA) is a derivative of the Boeing CH-47 Chinook, with extensive modifications to the fuel system, including greater capacity, air refueling (D and E only) and survivability improvements such as inert gas fillers for the fuel tanks. Eventually, all will be E models until remanufacture into the MH-60G.
The avionics have been enhanced for all-weather and night operations. Having a larger special operations helicopter gives U.S. Special Operations Command the ability to do behind-the-lines deliveries of vehicle-borne teams.
Current operations
While several Chinooks sank with the cargo ship Atlantic Conveyor, the Chinook was essential to the U.K. operations in the Falklands War.
The amount of load a cargo helicopter can carry depends on the model, the fuel on board, the distance to be flown, and atmospheric conditions.[1] In the high mountains of Afghanistan, these helicopters have done surprisingly well, while lighter helicopters' engines struggle.
CH-47's are in the Aviation Brigade of the new U.S. Army restructuring into brigades.
General characteristics
- Max Gross Weight: 50,000 lbs
- Empty Weight: 23,401 lbs
- Max Speed: 170 knots / 184 mph
- Normal Cruise Speed: 130 knots / 137 mph
- Rate of Climb: 1,522 ft/min
- Rotor System: three manual-folding blades per hub (two hubs); 225 revolutions per minute; 60-ft rotor span
- Troop Capacity: 36 (33 troops plus 3 crew members)
- Litter Capacity: 24
- Sling-load Capacity: 26,000 lb center hook; 17,000 lb forward/aft hook; 25,000 lb tandem
- Minimum Crew: 3 (pilot, co-pilot, and flight engineer)