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Military Helicopters Β·Sikorsky

R-4

American helicopter from the 1940s, first to be produced in quantity, used primarily in World War II for rescue operations.

Max speed
121km/h
Range
210km
Produced
131units
Avg unit price
$10K
Sikorsky R-4 military helicopters side profile drawing
Side profile Β· Sikorsky R-4 Β· length 10.8 m
Technical SpecificationsVersion: R-4
Crew1
Length10.8 m (35.4 ft)
Wingspan11.6 m (38.1 ft)
Height3.8 m (12.5 ft)
Empty weight950 kg (2,094 lbs)
Max. takeoff weight1,150 kg (2,535 lbs)
PerformanceVersion: R-4
Maximum speed121 km/h (75 mph)
Operational range210 km (130 mi)
Service ceiling2,400 m (7,874 ft)
Operators β€” 2026
No country is operating the R-4 in 2026.
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πŸ‡¨πŸ‡¦ CanadaΒ· πŸ‡¬πŸ‡§ United KingdomΒ· πŸ‡ΊπŸ‡Έ United States

Description

The Sikorsky R-4 was designed by Igor Sikorsky, evolving from his earlier experimental VS-300 helicopter, which had been publicly demonstrated in 1940. Designated initially as the XR-4 under the United States Army Air Forces' "Rotorcraft" series, it marked a significant step forward in rotary-wing aviation. The XR-4 first achieved flight on 14 January 1942, and was accepted by the Army on 30 May 1942. It exceeded all previous helicopter endurance, altitude, and airspeed records. This included a 761 mi (1,225 km) cross-country flight from Bridgeport, Connecticut, to Wright Field, Ohio, setting a helicopter peak altitude record of 12,000 ft (3,700 m), while achieving 100 flight hours without a major incident and top airspeed approaching 90 mph (78 kn; 145 km/h). Following this, the British Admiralty, having learned of the VS-300, made a ship available and the first deck-landing trials aboard Daghestan were carried out in 1944. The British received two of the first eight helicopters built. On 5 January 1943, the United States Army Air Forces ordered 29 prototypes. United Aircraft announced on 5 November 1944 that the one hundredth helicopter had been completed, and that the production rate had reached five every six days.

Design

The Sikorsky R-4 was designed with a single, three-bladed main rotor and was powered by a radial engine. The aircraft's blades were constructed with wood ribs around a steel spar and covered in doped fabric. These blades presented a challenge, as they were difficult to keep rotating in the same plane and vibrated excessively. There was no governor to control rotor speed, requiring the pilot to continuously correlate the throttle with collective pitch inputs. The aircraft operated with a gross weight of 2,540 lb (1,152 kg).

Armament

The R-4 was not designed as an attack or combat helicopter and consequently had very limited armament capabilities. While it could not carry bombs, missiles, or guns, the R-4B variant featured the capacity to carry one casualty litter externally. This external carriage was utilized for medical evacuation missions, demonstrating the helicopter's utility in rescue and support roles. Its primary role was focused on transport, rescue, and logistical support.

Operational History

The R-4 saw operational use in various theaters during World War II, marking the beginning of helicopter utility in military operations. Notably, it was deployed in the China-Burma-India theater where U.S. Army Lieutenant Carter Harman conducted the first combat rescue by helicopter, retrieving downed pilots and soldiers. It also supported Operation Ivory Soap in the South Pacific, ferrying parts between floating Aviation Repair Units, and undertaking medical evacuation and mercy missions. The R-4 demonstrated its value in difficult conditions, including high altitudes and humid climates. In British service, known as the Hoverfly, it contributed to helicopter training and development of rotor systems. The United States Coast Guard also used it in rescue missions, such as the delivery of blood plasma following the sinking of USS Turner. Despite its operational strengths, the R-4 had limitations, including a single-passenger capacity and inherent piloting difficulties stemming from blade vibrations and a lack of effective rotor speed control.

Variants

Main Variants:

  • XR-4: The initial prototype, designated Model VS-316A, featured a crew of two, dual controls, and a Warner R-500-3 165 hp engine.

  • YR-4A: This version incorporated a larger rotor diameter and a more powerful Warner R-550-1 180 hp engine, with three units manufactured for evaluation testing.

  • YR-4B: Featuring detailed design changes, this variant saw 27 units built for development testing, followed by an additional batch of 14, with seven being designated as HNS-1s for the US Navy.

  • R-4B: As the production version, it was equipped with a Warner R-550-3 200 hp engine, with 100 units manufactured, including 20 for the US Navy and 45 for the Royal Air Force.

  • HNS-1: This designation referred to three YR-4Bs and 22 R-4Bs transferred to the US Navy, with three units being diverted to the United States Coast Guard.

Frequently Asked Questions

What type of aircraft is the R-4?
The Sikorsky R-4 is a military helicopters aircraft developed by Sikorsky and entered service in 1944.
What is the maximum speed of the R-4?
The Sikorsky R-4 has a maximum speed of 121 km/h (75 mph).
What is the range of the R-4?
The Sikorsky R-4 has an operational range of 210 km (130 miles). This range can vary based on payload, altitude, and mission profile.
When did the R-4 first fly?
The Sikorsky R-4 made its first flight on January 13, 1942. It entered operational service in 1944.
How many R-4 have been built?
Approximately 131 units of the Sikorsky R-4 have been produced since it entered service in 1944.
How much does a R-4 cost?
The Sikorsky R-4 has an estimated unit cost of approximately $0.0 million. Actual prices vary based on configuration, quantity ordered, and included support packages.
What is the service ceiling of the R-4?
The Sikorsky R-4 has a service ceiling of 2,400 meters (7,874 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 23 July 2026. Suggest a change
Latest Data Updates
  1. JUL 232026 Updated Sources and cross-references refreshed
  2. APR 72026 Updated Sources and cross-references refreshed
  3. JAN 122026 Updated Range updated in a site-wide editorial pass