|R-5 / H-5|
|A Sikorsky YR-5A at the National Museum of the United States Air Force in Dayton, Ohio|
|First flight||18 August 1943|
|Primary users||United States Air Force|
|Number built||over 300|
|Developed from||Sikorsky R-4|
It was used by the United States Air Force, and its predecessor, the United States Army Air Forces, as well as the United States Navy and United States Coast Guard (with the designations HO2S and HO3S). It was also used by the United States Post Office Department.
In December 1946, an agreement was signed between the British company Westland Aircraft and Sikorsky to produce a British version of the H-5, to be manufactured under license in Britain as the Westland-Sikorsky WS-51 Dragonfly. By the time production ceased in 1951, more than 300 examples of all types of the H-5 had been built.
Design and developmentEdit
The H-5 was originally built by Sikorsky as its model S-48, designated as the R-5 by the United States Army Air Forces. It was designed to provide a helicopter having greater useful load, endurance, speed, and service ceiling than the Sikorsky R-4. The R-5 differed from the R-4 by having an increased rotor diameter and a new, longer fuselage for two persons in tandem, though it retained the R-4's tailwheel-type landing gear. Larger than the R-4 or the later R-6, the R-5 was fitted with a more powerful Wasp Junior 450-hp radial engine, and quickly proved itself the most successful of the three types. The first XR-5 of four ordered made its initial flight on 18 August 1943. In March 1944, the Army Air Forces ordered 26 YR-5As for service testing, and in February 1945, the first YR-5A was delivered. This order was followed by a production contract for 100 R-5s, outfitted with racks for two litters (stretchers), but only 34 were actually delivered. Of these, fourteen were the R-5A, basically identical with the YR-5A. The remaining twenty were built as the three-place R-5D, which had a widened cabin with a two-place rear bench seat and a small nosewheel added to the landing gear, and could be optionally fitted with a rescue hoist and an auxiliary external fuel tank. Five of the service-test YR-5As were later converted into dual-control YR-5Es. The United States Navy evaluated three R-5As as the HO2S-1.
Sikorsky soon developed a modified version of the R-5, the S-51, featuring a greater rotor diameter, greater carrying capacity and gross weight, and a redesigned tricycle landing gear configuration; this first flew on 16 February 1946. With room for three passengers plus pilot, the S-51 was initially intended to appeal to civilian as well as military operators, and was the first helicopter to be sold to a commercial user. Eleven S-51s were ordered by the USAF and designated the R-5F, while ninety went to the Navy as the HO3S-1, commonly referred to as the 'Horse'.
In Britain, Westland Aircraft began production in 1946 of the Westland-Sikorsky S-51 Dragonfly for the Royal Navy and the Royal Air Force, all of which were powered by a 500 hp Alvis Leonides engine. This gave an improved top speed of 103 mph and a service ceiling of 14,000 ft. In total, 133 Westland-Sikorsky Dragonfly helicopters were built. A considerably modified version was also developed by Westland as the Westland Widgeon, but the type was never adopted for service.
The U.S. Navy ordered four S-51s "off-the-shelf" from Sikorsky in late 1946 for use in the Antarctic and Operation Highjump, placing them into naval inventory as the HO3S-1. Carried aboard the seaplane tender USS Pine Island, on Christmas Day 1946 an HO3S-1 of VX-3 piloted by Lieutenant Commander Walter M. Sessums became the first helicopter to fly in the Antarctic. Having proved its capabilities, the initial naval HO3S-1 order was followed by subsequent purchases of an additional 42 aircraft in 1948. The Navy equipped several warship classes with HO3S-1 utility helos, including aircraft carriers, seaplane tenders, icebreakers, Des Moines-class cruisers, and Iowa-class battleships. By February 1948, the Marine Corps had equipped HMX-1, its first regular Marine Helicopter Transport Squadron, with six HO3S-1 aircraft. With a passenger load of only three lightly dressed persons, the HO3S-1s were primarily operated in the utility role by the marines; for the transport role, an additional nine tandem-rotor Piasecki-built HRP-1 helicopters were later added to the squadron. Eventually, the U.S. Navy would acquire a total of 88 HO3S-1 (S-51) helicopters.
Several H-5Hs were converted in 1949 to a unique medical-evacuation role, with casualty stretchers loaded sideways through blister-hatches on the side of the fuselage. The back stretcher station was located just forward of the tail boom and the main stretcher station was located behind the crew cabin. The forward stretcher station could accommodate two casualties, who were accessible to the medic in flight, while the back stretcher station handled only one, not accessible to the medic during the flight. Very little information is known about the operational use of this modification by the USAF, this being abandoned shortly after tests in 1950.
The R-5 had been designated under the United States Army Air Forces system, a series starting with R-1 and proceeding up to about R-16. In 1947 with the start of the United States Air Force, there was a new system, and many aircraft, but not all, were redesignated. The R-5 became the H-5. The United States Army broke off with its own designation system in the 1950s, resulting in new designations for its helicopter projects. In 1962 under the new tri-service system (see 1962 United States Tri-Service aircraft designation system), many navy and army aircraft were given the low numbers. Under the 1962 system, the low H numbers were given to new aircraft. For example, H-5 was given to the OH-5, a prototype design which never entered Army service.
During its service life, the H-5/HO3S-1 was used for utility, rescue, and mercy missions throughout the world, including flights during Operation Highjump in the Antarctic. While the extra power of the H-5 made it significantly more useful than its R-4 and R-6 cousins, the H-5/HO3S-1 suffered, like most early small tandem-seat single-rotor machines, from center of gravity problems. As a matter of routine, the helicopter was equipped with two iron-bar weights – each in a canvas case – one of 25 lb (11 kg) & one of 50 lb (23 kg). Flying with no passengers, both weights were placed forward alongside the pilot. With three passengers, both weights were normally placed in the baggage compartment. However, in conditions of high ambient temperatures, which reduced lift due to the lowered air density, all weights were jettisoned. If the weights could not be recovered later, pilots on future missions were forced to utilize rocks or other improvised weights next to the pilot after offloading three passengers, or else travel at a very slow 25 knots (46 km/h; 29 mph).
The H-5/HO3S-1 gained its greatest fame during the Korean War when it was called upon repeatedly to rescue United Nations pilots shot down behind enemy lines and to evacuate wounded personnel from frontline areas. It was eventually replaced in most roles by the H-19 Chickasaw. In 1957, the last H-5 and HO3S-1 helicopters were retired from active U.S. military service.
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- Prototype based on the VS.372 with two seats and tailwheel landing gear, powered by a 450hp R-985-AN-5, five built
- As the XR-5 with minor modifications, 26 built including two to the United States Navy as the HO2S-1
- Production rescue model with provision for two external stretchers, 34 built later re-designated H-5A
- Modified R-5A, not built
- Modified R-5A, not built
- Modified R-5As with nosewheel landing gear, rescue hoist, twenty conversion later re-designated H-5D
- Modified YR-5As with dual controls, five conversions later re-designated YH-5E
- Civil model S-51 four-seaters bought in 1947, 11 built later re-designated H-5F
- R-5A redesignated
- R-5D redesignated
- YR-5E redesignated
- R-5F redesignated
- Four-seater as H-5F with rescue equipment, 39 bought
- As H-5G with updated equipment, 16 built
- Two YR-5As to the United States Navy later passed to the United States Coast Guard, order for 34 cancelled
- Four-seat version for the USN similar to the H-5F, 88 built
- HO3S-1 for the United States Coast Guard, nine built
- Was a naval version of the H-5H, not built
- One HO3S-1 modified in 1950 with a redesigned rotor
- Civil four-seat transport version; four purchased for inventory for U.S. Navy
- See: Westland WS-51
- 43-46607/H1k-1/96 – YR-5A on display at the Royal Thai Air Force Museum, Don Muang Airport, Bangkok, Thailand
- 43-46620 – A YH-5A is on display at the National Museum of the United States Air Force at Wright-Patterson AFB near Dayton, Ohio. The aircraft is one of 26 ordered in 1944. It was obtained from Eglin Air Force Base, Florida, in March 1955.
- 43-46645 – H-5D on display at the United States Army Aviation Museum at Fort Rucker, Alabama.
- 43-47954 – An XR-5 is in storage with the National Air and Space Museum.
- 47-0484 – Carolinas Aviation Museum, Charlotte, North Carolina. Painted as bureau number 125136.
- 48-0548 – H-5G on display at the Pima Air & Space Museum adjacent to Davis-Monthan Air Force Base in Tucson, Arizona.
- 48-0558 – H-5G on display at the United States Army Aviation Museum at Fort Rucker, Alabama.
- 49-2007 – War Memorial of Korea, Seoul, Republic of Korea
- 122515 – HO3S-1 under restoration aboard the USS Midway Museum, San Diego, California. This airframe was at one point repaired using the tail boom from BuNo 124345. However, this tail boom was removed and replaced with the tail boom of a 3rd S-51.
- USCG 1232 – HO3S-1G on display at the Pima Air & Space Museum adjacent to Davis-Monthan Air Force Base in Tucson, Arizona. On loan from the United States Coast Guard.
- USCG 1233 – HO3S-1G at Evergreen Aviation & Space Museum, McMinnville, Oregon.
- USCG 1235 – HO3S-1G at the National Museum of Naval Aviation in Pensacola, Florida
- RCAF 9601 – A Dragonfly is on display at the National Air Force Museum of Canada in Trenton, Ontario.
- RCAF 9602 – H-5A (S-51) on display at the New England Air Museum, Bradley International Airport, Windsor Locks, Connecticut
- RCAF 9603 – American Helicopter Museum & Education Center, West Chester, Pennsylvania
- RCAF 9607 – An H-5 is on display at the Aero Space Museum of Calgary in Calgary, Alberta.
- JRV-11503/WA/H/97 An S-51 Mk-1B is on display at the Air Museum at Nikola Tesla Airport, Belgrade, Serbia
Data from United States Military Aircraft since 1909
- Crew: two
- Capacity: two stretchers in external panniers
- Length: 57 ft 1 in (17.40 m)
- Rotor diameter: 48 ft 0 in (14.63 m)
- Height: 13 ft 0 in (3.96 m)
- Disc area: 1,810 sq ft (168.2 m²)
- Empty weight: 3,780 lb (1,718 kg)
- Loaded weight: 4,825 lb (2,193 kg)
- Powerplant: 1 × Pratt & Whitney R-985 Wasp Junior, 450 hp (335 kW)
- R-5 until 1948 when use of R for "rotary-wing" was replaced by H "helicopter" under the designation system
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|Wikimedia Commons has media related to Sikorsky H-5.|
- "Westland-Sikorsky S-51", Flight, 1 April 1948
- Sikorsky S-48/R-5 and S-51/HO3S-1/H-5F, G, H pages at the Sikorsky Archives
- Sikorsky YH-5A page at the National Museum of the United States Air Force
- Sikorsky S-51 First Helicopter in Antarctica. – Argentinian Government. Link in Spanish – Google Translation in English
- Newsreel footage of a Sikorsky S-51 (1949) from British Pathé (Record No:26763) at YouTube
- AN 01-230HB-1 Handbook Flight Operating Instructions USAF Series H-5A, D, and E, Navy Model HO2S-1 Helicopters (1951)