Piasecki H-21
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 degrees F, and could be routinely maintained in severe cold weather environments.
Design and development
Piasecki Helicopter designed and successfully sold to the US 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 hit 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 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 9-cylinder Curtis-Wright R-1820-103 Cyclone supercharged 1150 hp air-cooled radial engine. After its maiden flight in April 1952, the Air Force 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 U.S. Air Force (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.
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.
Operational history
French Service in the Algerian War
A
Shawnee over rice paddies in
Vietnam.
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-Luftwaffe) MG 151/20 20 mm aircraft cannon for defensive use when landing assault forces under fire.[1][2][3]
Though the H-21 had been removed from the ground attack role, official 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 helos in large-scale counterinsurgency operations.[1][2][3]
U.S. Army Operations
The H-21C saw extensive service with the U.S. Army, primarily for use in transporting troops and supplies. On August 24, 1954, with the assistance of in-flight 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.[4] 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 ARVN (Army Republic South Vietnam) troops. In Army aviation 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 NVA and Viet Cong ground forces, which were increasingly well-supplied with automatic small arms and heavy (12.7 mm) AA machine guns. The shooting down of a CH-21 Shawnee near the Laotian-Vietnamese border with the death of four Army aviators in July 1962 were the U.S. Army's first Vietnam casualties.[5] 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 UH-1 Huey. In 1965, the 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.
Variants
Cockpit view of the H-21.
- XH-21
- US Air Force 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-Defence 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 licence 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.
- CH-21A
- H-21A redesignated in 1962.
- CH-21B
- H-21B redesignated in 1962.
- CH-21C
- H-21C redesignated in 1962.
- HH-21B
- 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 (as HKP-1), 2 for the Swedish Air Force, 9 for the Swedish Navy. 2 used for test/evaluation purposes by Japan Self-Defence Forces.
- Model 44B
- Commercial 15-passenger/freighter version of the H-21B.
- Model 44C
- Commercial eight-passenger executive version of the H-21B.
- CH-127
- Vertol Canada Model 44
Operators
HKP-1 in Swedish Navy markings
Military Operators
Canada
France
Germany
Japan
- Japan Air Self-Defence Force operated 10 H-21B helicopters as rescue .
- Japan Ground Self-Defense Force operated 2 Model 44A helicopters for testing.
Sweden
- Swedish Air Force operated HKP-1 helicopters.
- Swedish Navy operated HKP-1 helicopters.
United States
Civil Operators
Canada
United States
Survivors
Japan
- On display
- Model 44A JG-0002 at the Tokorozawa Aviation Museum, Tokorozawa.
United States
H-21B Shawnee 53-4347 on display at the Pueblo Weisbrod Aircraft Museum in Pueblo, Colorado in November 2007
CH-21B 53-4366 in
USAF markings at the Canadian Museum of Flight 1988
- Airworthy
- CH-21B N64606 the former 54-4001 operated by the Classic Rotors Museum, Ramona, California, the last H-21 still flown.[6][7]
- On display
- CH-21B 51-5857 at the National Museum of the United States Air Force, Wright Patterson AFB, Dayton, OH. It was obtained from Eglin Air Force Base in January 1965[8]
- CH-21B 51-5859 at the USS Alabama Museum in Mobile, AL
- CH-21C 51-5886 at Aerospace Museum of California
- CH-21B 51-5892 at Quonset Point, RI
- CH-21B 52-8676 at the Strategic Air and Space Museum, Ashland, NE
- CH-21B 52-8685 at the Museum of Aviation, Robins AFB, GA
- CH-21B 52-8688 at the Travis Air Museum, Travis AFB, CA
- CH-21B 52-8691 at Kirtland AFB, NM, marked as '34343'
- CH-21B 53-4324 at the Pate Museum of Transportation, Cresson, TX
- CH-21B 53-4326 at the March Field Air Museum, March ARB, CA
- CH-21B 53-4347 at the Pueblo Weisbrod Aircraft Museum, Pueblo, CO
- SH-21B 53-4362 at the Alaska Museum of Transportation and Industry, Wasilla, AK
- CH-21B 53-4366 at the Museum of Flight, Seattle, WA (previously at the Canadian Museum of Flight)
- CH-21B 53-4367 at the Mid-Atlantic Air Museum, Reading, PA
- CH-21B 53-4369 at the U.S. Army Aviation Museum, Fort Rucker, AL
- CH-21B 53-4389 at the Pima Air & Space Museum, Tucson, AZ
- CH-21B 54-4003 at the Florence Air & Missile Museum, Florence, SC
- CH-21B 54-4404 at the Alaska Aviation Heritage Museum, Anchorage, AK
- CH-21C 55-4140 at the Intrepid Sea-Air-Space Museum, New York, NY
H-21C at Wings Over the Rockies Museum
- CH-21C 55-4218 at the Wings Over the Rockies Air and Space Museum, Denver, CO, marked as 53-4379
- CH-21C 56-2040 at the U.S. Army Aviation Museum, Fort Rucker, AL
- CH-21C 56-2077 at the U.S. Army Transportation Museum, Fort Eustis, VA
- CH-21C 56-2142 at the Hill Aerospace Museum, Hill AFB, UT, marked as 54-4002
- CH-21C 56-2159 at the Pima Air & Space Museum, Tucson, AZ
- Stored or under restoration
- CH-21B 52-8623 in store at Edwards AFB, CA
- CH-21B 53-4329 at the Museum of Flight Restoration Center, Paine Field, Everett, WA
Specifications (CH-21C)
Data from U.S. Army Aircraft Since 1947 [9]
General characteristics
- Crew: 3–5 (Pilot, co-pilot, crew chief and one or two gunners in Vietnam)
- Capacity:
- 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 (6,609 kg)
- Powerplant: 1× Wright R-1820-103 radial engine, 1,425 hp (1,063 kW) driving 2 rotors
Performance
Armament
See also
Related development
Comparable aircraft
- Bristol Belvedere
- Yakovlev Yak-24
Related lists
- List of military aircraft of the United States
References
- ↑ 1.0 1.1 France, Operations Research Group, Report of the Operations Research Mission on H-21 Helicopter (1959)
- ↑ 2.0 2.1 Riley, David, French Helicopter Operations in Algeria, Marine Corps Gazette, February 1958, pp. 21-26
- ↑ 3.0 3.1 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.
- ↑ "FAA REGISTRY: N64606". Federal Aviation Administration. 11 November 2009. http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N64606. Retrieved 2009-11-12.
- ↑ Classic Rotors Museum (undated). "About Us". http://www.rotors.org/aboutus.htm. 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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