USA - Naval aviation and armament
Bell HUL (UH-13 / HH-13) utility / rescue helicopter
HUL-1 (UH-13J)
Modification | Purpose | Deliveries | Number of commissioned | Discarding | Differences from the previous modification |
HUL-1, 1962 - UH-13J | utility | 1/1957 - 3/1959 | 30 | 6/1973 | 3 passener |
HUL-1G (HH-13J) | rescue | rescue equipment |
Modification |
HUL-1 (UH-13J) |
Rotor diameter, m |
11.32 |
Length, m |
9.90 |
Height, m |
2.72 |
Rotating area, m2 |
100.59 |
Empty mass, kg |
734 |
Full flying-off mass, kg |
1270 |
Engine | 1 Avco Lycoming VO-435-A1 |
Power, h. p. | 240 |
Maximal speed, km/h | 169 |
Cruise speed, km/h | 143 |
Flying range, km | 416 |
Vertical speed, m/s | 4.1 |
Maximal altitude, m | 3415 |
Complement | 1 |
Armament | 3 passenger |
HUL-1 (UH-13J)
© Ivan Gogin, 2008