Saunders-Roe Skeeter
| Skeeter | |
|---|---|
 | |
| Skeeter | |
| Vloga | Lahki helikopter |
| Proizvajalec/-ci | Saunders-Roe |
| Krstni polet | 8. oktober 1948 (Cierva W.14) |
| Predstavljen | Oktober 1956 |
| Glavni uporabniki | Britanska kopenska vojska RAF Nemška kopenska vojska Nemčka mornarica |
Saunders-Roe Skeeter je bil dvosedežni enomotorni batnognani helikopter, ki ga je razvil britanski Saunders-Roe ("Saro") v 1940ih. Namenjen je bil šolanju pilotov in izvdniškim letom. Bil je prvi helikopter Zračnega korpusa britanske vojske (AAC).
Specifikacije (Skeeter AOP.12)
Podatki iz Saunders and Saro Aircraft since 1917<;London 1988, pp. 253–254.
Splošne karakteristike
- Posadka: 2
- Dolžina: 26 ft 8 in (8,12 m)
- Premer rotorja: 32 ft 0 in (9,75 m)
- Višina: 9 ft 6 in (2,89 m)
- Površina rotorjev: 804 ft² (74,7 m²)
- Teža praznega letala: 1656 lb (751 kg)
- Maks. vzletna teža: 2200 lb (998 kg)
- Pogon letala: 1 × 4-valjni zračnohlajeni batni motor de Havilland Gipsy Major 215, 215 KM (160 kW)
Zmogljivost
- Maks. hitrost: 109 mph (95 vozlov, 175 km/h)
- Potovalna hitrost: 106 mph (92 vozlov, 171 km/h)
- Doseg: 260 milj (226 nmi, 418 km)
- Trajanje leta: 3 ure
- Višina leta: 12800 ft (3901 m)
- Hitrost vzpenjanja: 1150 ft/min (5,8 m/s)
Glej tudi
Reference
Bibliografija
- "Cierva Skeeter Flies". Flight, 21 October 1948, pp. 477–478.
- London, Peter. "Last of the Line: The Saro Skeeter". Air Enthusiast, No. 54, Summer 1994. ISSN 0143-5450. pp. 2–5.
- London, Peter (1988). Saunders and Saro Aircraft since 1917. London: Putnam. ISBN 0-85177-814-3.
- "Saunders-Roe Skeeter: Development and Construction of the Mark Six". Flight, 30 March 1956. pp. 355–359, 374.
Zunanje povezave
Wikimedijina zbirka ponuja več predstavnostnega gradiva o temi: Saunders-Roe Skeeter.
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