|
||||||||||||||||
| The H-5, originally designated the R-5 (H for Helicopter; R for Rotorcraft), was designed to provide a helicopter having greater useful load, endurance, speed and service ceiling than the R-4. The first XR-5 of four ordered made its initial flight on Aug. 18, 1943. In March 1944 the AAF ordered 26 YR-5As for service testing, and in February 1945 the first YR-5A was delivered.
During its service life, the H-5 was used for rescue and mercy missions throughout the world. It gained its greatest fame, however, 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. More than 300 H-5s were built by the time production was halted in 1951. SPECIFICATIONS: Main rotor diameter: 48 ft. Tail rotor diameter: 8 ft. 5 in. Fuselage length: 41 ft. 2 in. Height: 12 ft. 11 in. Weight: 4,815 lbs. loaded Armament: None Engine: Pratt & Whitney R-985 of 450 hp PERFORMANCE: Maximum speed: 90 mph Cruising speed: 70 mph Range: 280 miles Service ceiling: 10,000 ft. |
|
|
| Bibliography: National Museum of the USAF |