Air Weapons

Observation (1945)

Sikorsky

R-5 Dragonfly

R-5 Dragonfly

The Sikorsky R-5 was the ultimate development of the basic R-4 observation and rescue helicopter that preceded it and was a considerably more radical departure from the original design than the R-6 that was produced concurrently. The R-5 was easily distinguished by an elongated fuselage with a tandem-seat arrangement in which the observer sat in front of the pilot. The main rotor was also considerably larger and powered by a radial engine with over twice the horsepower. Another notable difference was the tricycle landing gear which replaced the earlier tailwheel. The more powerful engines and larger fuselage allowed the R-5 to carry a heavier load than the R-4/6 and therefore made it useful as a utility helicopter for both land- and ship-based roles. As such, it was the first helicopter to operate in the Antarctic and served extensively in the Korean War. It was also license-built in Britain by Westland where it was known as the Dragonfly and served in Malaya. Other users included Argentina, Australia, Canada, China, France and South Africa. The last R-5s were retired from service in the late 1950s when they were replaced by the H-19.

First flight of the prototype XR-5 took place on 18 September 1943 and the first YR-5A was delivered in 1945 for testing. Production versions began with the R-5A which had provision for two stretchers, followed by the R-5D which were the first with a tricycle landing gear, and the R-5F which were based on the civil S-51. After 1948, all of these were redesignated H-6. Further versions included the H-6G four-seater and the updated H-6H, both of which had hydraulic boosted controls and untapered metal blades. Naval versions included the HO2S-1 prototype which was followed by the HO3S-1 four-seater. British versions began with the WS-51 evaluation version followed by the production Dragonfly HR.1, HR.3 and HR.5 for the Royal Navy and HC.2 and HC.4 for the RAF. All of these were fitted with more powerful Leonides engines and were primarily employed on rescue and casevac missions. Additional civilian versions were also built.

Preceded by:

None

Succeeded by:

None

Datafile

DesignR-5ADragonfly HR.1
NameDragonflyDragonfly
TypeUtilityUtility
Year19461950
Crew21-4
Dimensions
Length12.47 m12.47 m
Height3.940 m3.940 m
Rotor Diameter
Rotor Disc Area
Wing Span14.60 m14.94 m
Wing Arean/an/a
Weight
Empty1,710 kg1,724 kg
Maximum2,268 kg2,663 kg
Wing Loading13.5 kg/m²?
Performance
Speed144 km/h166 km/h
Ceiling4,389 m3,780 m
Range580 km482 km
Powerplant
Engine1 x R-985-4B
Pratt & Whitney
336 kW
1 x Leonides Mk 50
Alvis
403 kW
Thrust/Weight0.240.28
Armament
Guns--
Payload--
Production
Built3413
Total518
All: Total production, R-5 (379) and Dragonfly (139).

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