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Sikorsky CH-54 Tarhe

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American twin-engine heavy-lift helicopter

CH-54 Tarhe
General information
TypeHeavy-liftcargo helicopter
ManufacturerSikorsky AircraftErickson (1992-)
StatusRetired
Primary userUnited States Army
Number built105
History
First flight9 May 1962
Retired1970s (US Army)
1993 (National Guard)[1]
VariantsS-64 Skycrane

TheSikorsky CH-54 Tarhe is an American twin-engine heavy-lifthelicopter designed bySikorsky Aircraft for theUnited States Army. It is named afterTarhe, an 18th-century chief of theWyandot Indian tribe whose nickname was "The Crane".[2] The civilian version is theSikorsky S-64 Skycrane.

Development

[edit]
A CH-54A Tarhe carrying a pair ofUH-1 Hueyutility helicopters
CH-54B carrying anM551 Sheridan tank,Redstone Arsenal, Alabama
Sikorsky Skycrane CH-54B with landing gear modified for soft ground.

Work on what would become the CH-54 can be traced back to Sikorsky's earlier activities with "sky-crane"helicopters, particularly thepiston-enginedSikorsky S-60 of the late 1950s. Following the end of theKorean War, theUnited States Army sought to procure a successor to theSikorsky CH-37 Mojave, an early piston-engined heavy lift helicopter; being aware of this need, Sikorsky were keen to fulfill it.[1] The company was already working on theSikorsky S-64 Skycrane, a civil-orientated heavy lift rotorcraft that was designed specifically for the purpose of carrying large payloads externally; the development of a military-configured derivative was viewed as a natural option. While Sikorsky were quick to recognise the advantages of adoptingturboshaft propulsion, there were no suitable engines of that type initially available, thus it had to work with the American engine manufacturerPratt and Whitney to modify theirJT12turbojet to produce one.[1]

One innovative feature for any helicopter of the era was the incorporation of an automaticflight control system, effectively afly-by-wire arrangement.[1] This feature enabled the aft-facing crew member to control the rotorcraft'spitch,roll, andyaw with 10% control authority, along with an altitude-hold function; it was also praised for being relatively easy to fly underinstrument flight rules (IFR).[1] Considerable attention was paid to the fuselage's design, particularly to minimising weight and maintenance requirements. Thelanding gear was designed to kneel to make loading easier as well as to ease operations from sloped surfaces.[1] From on onset, Sikorsky sought to enable the type to carry as diverse a range of cargoes as possible, leading to the incorporation of fitting for the carriage ofbarges and of a specially-designed multipurpose "people pod" that was suited for use for personnel transport,paratroop operations, and even as a mobile hospital or mobile command post.[1][3]

On 9 May 1962, the first of three prototypes performed itsmaiden flight.[4] It was subsequently tested by the US Army atFort Benning while the other two underwent an evaluation inWest Germany.[1] During June 1963, it was announced that the US Army had placed an order for an initial six helicopters, designating it as theCH-54A; the first of these was officially accepted on 30 June 1963.[1] Following a relatively brief period of testing and evaluation, the CH-54 was quickly put into active use in Vietnam.[1]

Early on, the type had demonstrated itself to possess unrivalled performance in some aspects. As of 2014[update], it continues to hold the helicopter record for highest altitude in level flight at 11,000 m (36,000 ft), which it set in 1971,[5] as well at the fastest climb to 3,000,[6] 6,000,[7] and 9,000[8] m (10,000, 20,000, and 30,000 ft). On 20 April 1965, a CH-54A equipped with a people pod lifted 90 people, comprising its crew of three and 87 combat-equipped troops; this was the largest number of people to be lifted by a single helicopter at that time.[1]

Operational history

[edit]

The United States Army would ultimately procure 105 examples, which it operated under the designation ofCH-54 Tarhe. It was most prolifically used during theVietnam War, typically to provide logistical support and heavy transport activities in aid of American ground troops. In the theater, CH-54s would routinely be used to reposition artillery pieces such as theM101 howitzer, and even airlift bulky payloads such asbulldozers andpatrol boats.[9][10] In terms of retrieved aircraft alone, in excess of 380 were reportedly recovered via CH-54, resulting in the saving of several hundred million dollars.[1][3]

In particular, those forces operating in and around theDemilitarized Zone (DMZ) betweenNorth Vietnam andSouth Vietnam were unable to rely on ground supply routes due to the unavoidable challenges posed by the local geography; instead, they were almost entirely dependent on air support provided by rotorcraft such as the CH-54.[11] The type would operate so close to the frontlines that several would come under fire from the North Vietnamese.[12][13] One unusual use of the type came under theCombat Trap programme, which saw it drop 10,000 lb bombs, intended for clearing landing zones.[1] One danger that its crews had to maintain awareness of was the strong downwash generated by the rotors; nearby tents were particularly at risk of being blown away.[14]

As a heavy transport helicopter, capable of retrieving numerous types of downed aircraft, it proved to be highly successful. The Tarhe can hold its cargo up and tight against its center spine to lessen drag and eliminate the pendulum effect when flying forward, as well as winch vehicles up and down from a hovering position, so the helicopter can deploy loads while hovering. Due to budget cuts, theHeavy Lift Helicopter (HLH) program was canceled and the CH-54 was not upgraded with larger engines. The relatively small fleet proved costly to maintain, thus the tandem-rotorBoeing CH-47 Chinook, a rival heavy lift helicopter, gradually supplemented the CH-54 for most transport duties, eventually replacing it in Regular Army aviation units during the 1980s. Another heavy lift helicopter, theSikorsky CH-53 Sea Stallion, had also been developed using many of the proven systems of the CH-54, including its engine, fuselage, and dynamic systems.[15]

The CH-54 was also operated by theArmy National Guard, where it performed a variety of military and civilian missions.[1] It participated in various humanitarian relief operations, including the rescuing of awhale inAlaska. Unusual payloads include whole antenna towers andlog cabins; another example was the use of a CH-54 to airliftair conditioners onto the roof of thePentagon.[1] Furthermore, it was commonly tasked with relocating non-airworthy or retired aircraft. Despite these atypical demands, the CH-54 achieved a strong safety record.[1] The military cutbacks enacted at the end of theCold War proved to be the death knell for the CH-54's military service; the final National Guard flight was conducted on 10 January 1993.[1]

Following their withdrawal from military use, many CH-54s were acquired by civilian operators and thus continued to be used in this new capacity.[1] Of these,Erickson Air-Crane ofCentral Point, Oregon, operates the largest fleet of S-64 helicopters in the world under the nameErickson S-64 Aircrane. These can be equipped withwater-dropping equipment (some also have foam/gel capability) forfirefighting duties worldwide.[16] After obtaining the type certificate and manufacturing rights in 1992, Erickson remains the manufacturer.

Variants

[edit]
YCH-54A
Preproduction aircraft, six built.[17]
CH-54A
Production model powered by two 4,500 shp (3,400 kW)Pratt & Whitney T73-P-1 turboshafts, 54 built.[17]
CH-54B
Heavier version of the CH-54A with two 4,800 shp (3,600 kW) T73-P-700 turboshafts and twin-wheeled main undercarriage, 37 ordered, 29 built.[18][1]
S-64B
In 1968, Sikorsky proposed a three-engined growth version with upgraded rotor and gearbox. This was not proceeded with but did form the basis for theCH-53E Super Stallion.[19]

Operators

[edit]
US Army CH-54A Tarhe (S-64A), 1989
 United States

Surviving aircraft

[edit]
CH-54A Tarhe ("Skycrane") on display
Main article:List of surviving Sikorsky CH-54s

A large number of surviving airframes exist in flyable condition as well as in museum collections worldwide.

Specifications (CH-54B)

[edit]
Orthographically projected diagram of the Sikorsky CH-54B Tarhe.
Orthographically projected diagram of the Sikorsky CH-54B Tarhe.

General characteristics

  • Crew: 3
  • Capacity: 25,000 lb (11,340 kg) payload
  • Length: 88 ft 6 in (26.97 m)
  • Height: 25 ft 5 in (7.75 m)
  • Empty weight: 19,800 lb (8,981 kg)
  • Max takeoff weight: 47,000 lb (21,319 kg)
  • Powerplant: 2 ×Pratt & Whitney T73-P-700turboshaft engines, 4,800 shp (3,600 kW) each
  • Main rotor diameter: 72 ft 0 in (21.95 m)
  • Main rotor area: 4,071.5 sq ft (378.25 m2) *Blade section:NACA 0011 mod[25]

Performance

  • Maximum speed: 130 kn (150 mph, 240 km/h)
  • Cruise speed: 100 kn (120 mph, 190 km/h)
  • Range: 200 nmi (230 mi, 370 km)
  • Rate of climb: 1,330 ft/min (6.8 m/s)

See also

[edit]

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

[edit]

Citations

[edit]
  1. ^abcdefghijklmnopqrsChandler, James T (1994)."And then there were none!".United States Army Aviation Digest. U.S. Government Printing Office.
  2. ^"Tarhe".Ohio History Central.
  3. ^abSikorsky 2007, p. 95.
  4. ^Taylor 1976, p. 386.
  5. ^"FAI Record ID #9918 – Altitude in horizontal flight. Class E-1 (Helicopters), turbine".Fédération Aéronautique Internationale. Archived fromthe original on 5 January 2015. Retrieved21 September 2014.
  6. ^"FAI Record ID #9942 – Time to climb to a height of 3 000 m. Class E-1 (Helicopters), turbine".Fédération Aéronautique Internationale. Archived fromthe original on 23 June 2015. Retrieved21 September 2014.
  7. ^"FAI Record ID #9957 – Time to climb to a height of 6 000 m. Class E-1 (Helicopters), turbine".Fédération Aéronautique Internationale. Archived fromthe original on 23 June 2015. Retrieved21 September 2014.
  8. ^"FAI Record ID #9960 – Time to climb to a height of 9 000 m. Class E-1 (Helicopters), turbine".Fédération Aéronautique Internationale. Archived fromthe original on 24 June 2015. Retrieved21 September 2014.
  9. ^Wiest and McNab 2015, pp. 90, 95.
  10. ^Wise 2010, pp. 85–86.
  11. ^Wiest and McNab 2015, p. 92.
  12. ^Wise 2010, p. 88.
  13. ^Boyne 2011, p. 146.
  14. ^Tucker 2011, p. 470.
  15. ^Boyne 2011, pp. 276–277.
  16. ^Boyne 2011, p. 336.
  17. ^abHarding 1990, p. 243.
  18. ^"CH-54B Tarhe".Helis.com. Retrieved30 July 2017.
  19. ^"S-64 Skycrane (CH-54 Tarhe)".sikorskyarchives.com. Retrieved30 July 2017.
  20. ^"What Is a Helicopter?". nasa.gov. Retrieved26 January 2013.
  21. ^"Sikorsky CH – 54B Skycrane Helicopter". nasa.gov. Archived fromthe original on 16 February 2013. Retrieved26 January 2013.
  22. ^"Sikorsky CH-54 Tarhe Flying crane". Military-Today.com. Archived from the original on 16 February 2013. Retrieved26 January 2013.
  23. ^abcdefghi"Sikorsky S-64 Skycrane / Sikorsky CH-54 Tarhe".all-aero.com.
  24. ^"Aviation Photo Search".
  25. ^Lednicer, David."The Incomplete Guide to Airfoil Usage".m-selig.ae.illinois.edu. Retrieved16 April 2019.

Bibliography

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External links

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