|USAF CH-21B at the National Museum of the United States Air Force.|
|Status||retired from active service|
|Primary users||United States Air Force
United States Army
French Army Aviation
|Developed from||HRP Rescuer|
The Piasecki H-21 Workhorse/Shawnee is an American helicopter, the fourth of a line of tandem rotor helicopters designed and built by Piasecki Helicopter (later Boeing Vertol). Commonly called the "flying banana", it was a multi-mission helicopter, utilizing wheels, skis, or floats.
The H-21 was originally developed by Piasecki as an Arctic rescue helicopter. The H-21 had winterization features permitting operation at temperatures as low as −65 °F (−54 °C), and could be routinely maintained in severe cold weather environments.
- 1 Design and development
- 2 Operational history
- 3 Variants
- 4 Operators
- 5 Aircraft on display
- 6 Specifications (CH-21C)
- 7 See also
- 8 References
- 9 External links
Design and development
Piasecki Helicopter designed and successfully sold to the United States Navy a series of tandem rotor helicopters, starting with the HRP-1 of 1944. The HRP-1 was nicknamed the "flying banana" because of the upward angle of the aft fuselage that ensured the large rotors did not strike each other in flight. The name would later be applied to other Piasecki helicopters of similar design, including the H-21.
In 1949, Piasecki proposed the YH-21A Workhorse to the United States Air Force (USAF), which was an improved, all-metal derivative of the HRP-1. Using two tandem, fully articulated three-bladed counter-rotating rotors, the H-21 was powered by one nine-cylinder Curtis-Wright R-1820-103 Cyclone supercharged 1,150 hp (858 kW) air-cooled radial engine. After its maiden flight in April 1952, the USAF ordered 32 H-21A SAR models and 163 of the more powerful H-21B assault transport variant. The H-21B was equipped with an uprated version of the Wright 103 engine, developing 1425 shaft horsepower (1063 kW), and featured rotor blades extended by 6 inches (152 mm). With its improved capabilities, the H-21B could carry 22 fully equipped infantrymen, or 12 stretchers, plus space for two medical attendants, in the medevac role. With its Arctic winter capabilities, the H-21A and H-21B were put into service by both the USAF and the Royal Canadian Air Force (RCAF) to maintain and service DEW (Distant Early Warning) radar installations stretching from the Aleutian Islands and Alaska across the Canadian Arctic to Greenland and Iceland.
In 1952, some H-21As were evaluated by USMC helicopter squadron HMX-1 in the air assault role. In 1957, an H-21B was loaned to the United States Marine Corps (USMC) to evaluate the helicopter as an airborne tug to tow disabled landing ships and amphibious landing vehicles to the beach. During the evaluation, the H-21B towed an LST at 5 knots and a simulated tracked amphibious vehicle from the water to the beach.
The uprated 1425 hp Wright engine used in the H-21B was also used in subsequent variants sold to both the U.S. Army (as the H-21C Shawnee) and the military forces of several other nations. In 1962, the H-21 was redesignated the CH-21 in U.S. Army service.
In 1959 Vertol Aircraft, who had acquired Piasecki, came up with a concept for heavy lift over short distances where between two to six H-21Bs would linked by beams to lift heavy loads. It was considered to be unsafe, because if one helicopter had mechanical problems during the lift it could cause an unbalanced situation and cause all helicopters to crash.
French service in the Algerian War
In 1956, seeking a way to use helicopters in a ground-attack role in the Algerian War, the French Air Force and French Army Aviation (ALAT, Aviation Légère de l'Armée de Terre) experimented with arming the Sikorsky S-55, then being superseded in service by the more capable Piasecki H-21 and Sikorsky H-34 helicopters. Some French Air Force and Army aviation H-21C helicopters were subsequently armed with fixed, forward-firing rockets and machine guns. A few even had racks for bombs, but tests subsequently determined that the H-21C lacked the maneuverability and performance needed in the ground-attack role. The H-21C was far more successful as a troop transport, and most H-21Cs in service were eventually fitted with flexible door-mounted guns such as the .50 cal. (12.7 mm) Browning machine gun or the (ex-German) MG 151/20 20 mm aircraft cannon for defensive use when landing assault forces under fire.
Though the H-21 had been removed from the ground-attack role, official U.S. Army evaluations at the time indicated that the type was actually more likely to survive multiple hits by ground fire than was the Sikorsky CH-34; this was assumed to be a consequence of the location and construction of the CH-34's fuel tanks. By the close of the Algerian War, troop-carrying H-21C helicopters were being used in concert with H-34 ground-attack helicopters in large-scale counterinsurgency operations.
U.S. Army operations
The H-21C saw extensive service with the U.S. Army, primarily for use in transporting troops and supplies. On 24 August 1954, with the assistance of inflight refueling provided by a U.S. Army U-1A Otter, a H-21C known as Amblin' Annie became the first helicopter to cross the United States nonstop. Various experiments were made by the Army in arming the H-21C as a gunship; some Shawnees were armed with flex guns under the nose, while others were fitted with door guns. One experimental version was tested stateside with a Boeing B-29 Superfortress .50 cal. remote turret mounted beneath the nose. The H-21C (later designated CH-21C) was first deployed to Vietnam in December 1961 with the Army's 8th and 57th Transportation Companies, in support of Army of the Republic of Vietnam troops. In Army service, the CH-21C Shawnee could be armed with 7.62 mm (.308 in) or 12.7 mm (.50 in) flexible door guns. Relatively slow, the CH-21's unprotected control cables and fuel lines proved vulnerable to the enhanced threat posed by North Vietnamese Army and Vietcong ground forces, which were increasingly well supplied with automatic small arms and heavy (12.7 mm) AA machine guns. The H-21, which was designed for cold weather operations, performed poorly in the hot weather of Vietnam. Despite being capable of carrying 20 passengers, it carried only nine when operating in Vietnam. The shooting down of a CH-21 Shawnee near the Laotian-Vietnamese border with the death of four aviators in July 1962 were some of the U.S. Army's earliest Vietnam casualties. Despite these events, the Shawnee continued in service as the U.S. Army's helicopter workhorse in Vietnam until 1964 when it was replaced with the Bell UH-1 Huey. In 1965, the Boeing CH-47 Chinook was deployed to Vietnam, and later that year, most CH-21 helicopters were withdrawn from active inventory in the U.S. Army and Air Force.
- USAF designation of the first H-21 prototype.
- YH-21 Work Horse
- USAF Search And Rescue (SAR) version of the HRP-2 for service test, eighteen built
- H-21A Work Horse (Model 42)
- Same as YH-21 with detailed changes and powered by one 1250hp Wright R-1820-102, re-designated CH-21A in 1962, 32 built for USAF, 6 for the Royal Canadian Air Force)
- H-21B Work Horse (Model 42)
- Same as H-21A but with uprated Wright engine (1425hp) and seats for 20 troops, autopilot as standard and limited armour protection and external fuel tanks, became CH-21B in 1962, 163 built for U.S. forces. 10 built for Japanese Self-Defense Forces; 10 H-21B built for the French Navy.
- SH-21B Work Horse
- Rescue conversion of the H-21B, became HH-21B in 1962.
- H-21C Shawnee (Model 43)
- US Army version of the H-21B, became CH-21C in 1962, 334 built for U.S. forces. 32 built under license by Weser Flugzeugbau for the West German Army. 98 built for the French Air Force and French Army Aviation (ALAT).
- XH-21D Shawnee (Model 71).
- Two H-21Cs re-engined with two General Electric T58 turboshaft engines in place of the Wright R-1820. Not placed into production.
- H-21A redesignated in 1962.
- H-21B redesignated in 1962.
- H-21C redesignated in 1962.
- SH-21B redesignated in 1962.
- Model 42A
- Conversion by Vertol Aircraft (Canada) of eight Royal Canadian Air Force H-21s for civilian use. Equipped to carry 19 passengers or 2,820lb (1,279kg) of internal cargo or a 5,000lb (2,268kg) slung load.
- Model 44A
- Commercial 19-passenger transport version of the H-21B. 11 total (Swedish military designation: Hkp 1), 2 for the Swedish Air Force, 9 for the Swedish Navy. 2 used for test/evaluation purposes by Japan Self-Defense Forces.
- Model 44B
- Commercial 15-passenger/freighter version of the H-21B.
- Model 44C
- Commercial eight-passenger executive version of the H-21B.
- Vertol Canada Model 44
- Piasecki HkP1
- Piasecki modell 44 for the Swedish Navy
Aircraft on display
|This section does not cite any references (sources). (April 2014)|
- Model 44A JG-0001 at the Bihoro air park, Hokkaido.
- Model 44A JG-0002 at the Tokorozawa Aviation Museum, Tokorozawa.
- H-21B 02-4756 at the Hamamatsu publicity hall, Hamamatsu Air Base.
- H-21B 02-4759 at the Gifu Air Field, Gifu.
- Model 44A N74056 at Central Air Force Museum in Monino, Moscow area. U.S. Vice President Richard Nixon gave it as a gift to Soviet premier Leonid Brezhnev.
- CH-21B 54-4001 operated as N64606 by the Classic Rotors Museum, Ramona, California, the last H-21 still flown.
- Static Display
- CH-21B 51-5857 at the National Museum of the United States Air Force, Wright-Patterson Air Force Base, Dayton, Ohio. It was obtained from Eglin Air Force Base in January 1965
- CH-21B, AF Ser. No. 51-5859 at the USS Alabama Museum in Mobile, Alabama
- CH-21C, AF Ser. No. 51-5886 at Aerospace Museum of California
- CH-21B, AF Ser. No. 51-5892 at Quonset Air Museum, Quonset State Airport (former NAS Quonset Point), Rhode Island
- CH-21B, AF Ser. No. 52-8676 at the Strategic Air and Space Museum, adjacent to Offutt AFB in Ashland, Nebraska
- CH-21B, AF Ser. No. 52-8685 at the Museum of Aviation, Robins Air Force Base, Georgia
- CH-21B, AF Ser. No. 52-8688 at the Travis Air Museum, Travis Air Force Base, California
- CH-21B, AF Ser. No. 52-8691 at Kirtland Air Force Base, New Mexico, marked as "34343"
- CH-21B, AF Ser. No. 52-8696 at Joint Base Elmendorf-Richardson (Elmendorf AFB), Alaska
- CH-21B, AF Ser. No. 53-4324 at the Vintage Flying Museum, Fort Worth, Texas
- CH-21B, AF Ser. No. 53-4326 at the March Field Air Museum, March Air Reserve Base (former March AFB), California
- CH-21B, AF Ser. No. 53-4347 at the Pueblo Weisbrod Aircraft Museum, Pueblo, Colorado
- SH-21B, AF Ser. No. 53-4362 at the Alaska Museum of Transportation and Industry, Wasilla, Alaska
- CH-21B, AF Ser. No. 53-4366 at the Museum of Flight, Seattle, Washington (previously at the Canadian Museum of Flight)
- CH-21B, AF Ser. No. 53-4367 at the Mid-Atlantic Air Museum, Reading, Pennsylvania
- CH-21B, Army Ser. No. 53-4369 at the U.S. Army Aviation Museum, Fort Rucker, Alabama
- CH-21B, AF Ser. No, 53-4389 at the Pima Air & Space Museum, adjacent to Davis-Monthan Air Force Base in Tucson, Arizona
- CH-21B 54-4003 at the Florence Air & Missile Museum, Florence, South Carolina
- CH-21B 54-4404 at the Alaska Aviation Heritage Museum, Anchorage, Alaska
- CH-21C 55-4140 at the Intrepid Sea, Air & Space Museum, New York, New York
- CH-21C 55-4218 at the Evergreen Aviation & Space Museum, McMinnville, Oregon (previously at the Wings Over the Rockies Air and Space Museum, Denver, Colorado), marked as 53-4379
- CH-21C, Army Ser. No. 56-2040 at the U.S. Army Aviation Museum, Fort Rucker, Alabama
- CH-21C 56-2077 at the U.S. Army Transportation Museum, Joint Base Langley–Eustis, Virginia
- CH-21C 56-2142 at the Hill Aerospace Museum, Hill Air Force Base, Utah, marked as 54-4002
- CH-21C 56-2159 at the Pima Air & Space Museum, adjacent to Davis-Monthan AFB in Tucson, Arizona
- Stored or under restoration
- CH-21B 52-8623 in storage at Edwards Air Force Base, California
- CH-21B 53-4329 under restoration at the Museum of Flight Restoration Center, Paine Field, Everett, Washington
Data from U.S. Army Aircraft Since 1947 
- Crew: 3–5 (Pilot, co-pilot, crew chief and one or two gunners in Vietnam)
- 20 troops or
- 12 stretchers
- Length: 52 ft 6 in (16.01 m)
- Rotor diameter: 44 ft 0 in (13.41 m)
- Height: 15 ft 9 in (4.80 m)
- Disc area: 3,041 ft² (282.6 m²)
- Empty weight: 8,950 lb (4,058 kg)
- Loaded weight: 15,200 lb (6,893 kg)
- Max. takeoff weight: 15,200 lb (6,893 kg)
- Powerplant: 1 × Wright R-1820-103 radial engine, 1,425 hp (1,063 kW) driving 2 rotors
- Maximum speed: 127 mph (110 knot, 204 km/h)
- Cruise speed: 98 mph (85 knots, 158 km/h)
- Range: 265 mi (230 nmi, 427 km)
- Service ceiling: 9,450 ft (2,880 m)
- Disc loading: 5 lb/ft² (24 kg/m²)
- Power/mass: 0.09 hp/lb (150 W/kg)
- Related development
- Aircraft of comparable role, configuration and era
- Related lists
- "Here Comes the Leathernecks." Popular Mechanics, April 1952, p. 101, bottom of page.
- "Flying Salvage Craft Works on Land Or Sea." Popular Mechanics, July 1957, p. 106
- "Workhorses of the Air." Popular Mechanics, March 1959, p. 100.
- France, Operations Research Group, Report of the Operations Research Mission on H-21 Helicopter (1959)
- Riley, David, French Helicopter Operations in Algeria, Marine Corps Gazette, February 1958, pp. 21-26
- Shrader, Charles R. The First Helicopter War: Logistics and Mobility in Algeria, 1954-1962 Westport, CT: Praeger Publishers (1999)
- The New Propwash, Fox Valley Sport Aviation Assoc., Vol.2, Issue 12, p. 5
- Harding 1990, pp. 261–262.
- "World Air Forces 1955 pg. 621". flightglobal.com. Retrieved 10 February 2015.
- H-21 "Flying the American Vertol 44 pg. 844" Check
|url=scheme (help). flightglobal.com. Retrieved 10 February 2015.
- "Helicopter World Market 1968 pg. 51". Flightglobal Insight. Retrieved 10 February 2015.
- "aéronautique navale H-21". helis.com. Retrieved 5 January 2013.
- "Helicopter World Market 1968 pg. 51". Flightglobal Insight. Retrieved 10 February 2015.
- "Helicopter World Market 1968 pg. 55". flightglobal.com. Retrieved 10 February 2015.
- "USAF H-21". helis.com. Retrieved 5 January 2013.
- "World Air Forces 1955 pg. 668". flightglobal.com. Retrieved 10 February 2015.
- "Helicopters in Civil Operations pg. 388". flightglobal.com. 21 March 1958. Retrieved 10 February 2015.
- "Hkp 1 - Flygvapenmuseum". Flygvapenmuseum.se. 2010-04-21. Retrieved 2012-12-17.
- "FAA REGISTRY: N64606". Federal Aviation Administration. 11 November 2009. Retrieved 2009-11-12.
- Classic Rotors Museum (n.d.). "About Us". Retrieved 2009-11-13.
- United States Air Force Museum (1975 edition)
- Harding 1990, p.262.
- Duke, R.A., Helicopter Operations in Algeria [Trans. French], Dept. of the Army (1959).
- Harding, Stephen. U.S. Army Aircraft Since 1947. Shrewsbury, UK:Airlife Publishing, 1990. ISBN 1-85310-102-8.
- United States Air Force Museum (1975 edition)
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