France - naval aviation and armaments
CH-21C
Modification | Purpose | Deliveries | Number of commissioned | Discarding | Differences from the previous modification |
H-21C | transport | 1956 | 13 | 1960 | --- |
Modification |
H-21C |
Rotor diameter, m |
2 x 13.41 |
Length, m |
15.98 |
Height, m |
4.70 |
Rotating area, m2 |
282.51 |
Empty mass, kg |
3629 |
Full flying-off mass, kg |
6668 |
Engine | 2 Wright R-1820-103 |
Power, h. p. | 2 x 1425 |
Maximal speed, km/h | 211 |
Cruise speed, km/h | |
Flying range, km | 644 |
Vertical speed, m/s | |
Maximal altitude, m | 2360 |
Complement | 2 |
Armament | 20 passengers or 2130 kg cargo in cabin |
H-21C
© Ivan Gogin, 2009