| General Information | ||
|---|---|---|
| Type | Ka-18 | |
| Function | Utility | |
| Year | 1956 | 1960 |
| Crew | 1 or 2 | |
| Powerplant (1) | ||
| Type | AI-14V | AI-14VF |
| Power | 255hp | 275hp |
| Size | ||
| Length (fuselage) | 7.03m | |
| Height | ?m | |
| Rotor Diameter | 9.96m | |
| Weights (kg) and loads | ||
| Empty | 1040 | 1032 |
| Loaded | 1460 | 1502 |
| Disc load | 18.71 | 19.25 |
| Power load (kg/hp) | 5.73 | 5.46 |
| Speed (km/h) | ||
| Maximum | 145 | 160 |
| Range (km) | ||
| Practical | ? | 300 to 750 |
| Ceiling (m) | ||
| Service | 3000 | 3500 |
| Payload | ||
| Fuel (internal) | 176l | |
| Fuel (external) | 2*70l | |
| Cargo | 350kg | 450kg |
| Seats | ||
Stretched version of Ka-15/ Ka-15M. In the original Ka-18 configuration, only fuselage design was revised: length was increased by 1.13m to enable ambulance stretcher to be carried internally. In passenger version added room could be used for additional passenger(s) and/or baggage. Fuselage cover - all metal, ply elements seen at Ka-15 finally abandoned. Sliding panels of the predecessor was replaced by large car-type doors.
To balance this the rear fuselage was extended and fin area increased. Engine, transmission, rotors, control system and undercarriage were same as on Ka-15. Since the powerplant was not changed, additional weight of enlarged fuselage had to be compensated by smaller fuel capacity.
Cabin heating, liquid de-icing for the rotor and windscreen, compressed air engine starter and all-weather instrumentation added much to helicopter functionality in harsh climate of the Soviet North. Ka-18 rotor blades were detachable for stowage - very useful for shipborn ice or fishery reconnaissance, or on warships. Without rotors Ka-18 measures only 7.03x2.84x3.35m3.
Ka-18 could be converted by adding/removing special equipment to fulfill following duties:
First experimental Ka-18 was flown October 13 1956 by pilot D.K.Efremov. Production at Ulan-Ude was launched in 1958. Ka-18 made appearance at number of International Air Shows (New-York, Mexico, Havana, Prague et al). In 1958 at Brussels helicopter won the Golden Medal.
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In 1960 boosted version of the AI-14V engine became available. Extra horsepowers allowed to increase payload by 100kg and operational ceiling by 500m. New modification carried same Ka-18 designation and could be identified by increased tailfin chord.
In May 1959 Ka-18 established a speed record (169.3km/h) on 500km closed circuit.
Known service: Moldavian and Ukrainian Directorates of Aeroflot;
About 200 built.
| Drawing of early production (small fins) Ka-18 from Virtual Aircraft Museum
Used for background on this page. |
| References | Links | |
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| Created January 25, 1996
Modified April 27, 2000 |
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