| Název: Name: | SAAB 91B Safir | SAAB 91B Safir |
| Originální název: Original Name: | SAAB 91B Safir | |
| Kategorie: Category: | víceúčelový letoun | utility aeroplane |
| Výrobce: Producer: | DD.MM.1949-DD.MM.195R Svenska Aeroplan AB, Linköping DD.MM.1951-DD.MM.1955 NV Koninklijke Maatschappij De Schelde, Dordrecht | |
| Období výroby: Production Period: | DD.MM.1949-DD.MM.195R | |
| Vyrobeno kusů: Number of Produced: | 25 SAAB 109 De Schelde | |
| První vzlet: Maiden Flight: | 18.01.1949 | |
| Osádka: Crew: | 1 + 2 | |
| Základní charakteristika: Basic Characteristics: | ||
| Vzlet a přistání: Take-off and Landing: | CTOL - konvenční vzlet a přistání | CTOL - conventional take-off and landing |
| Uspořádání křídla: Arrangement of Wing: | jednoplošník | monoplane |
| Uspořádání letounu: Aircraft Concept: | klasické | conventional |
| Podvozek: Undercarriage: | zatahovací | retractable |
| Přistávací zařízení: Landing Gear: | kola | wheels |
| Technické údaje: Technical Data: | ||
| Hmotnost prázdného letounu: Empty Weight: | 730 kg | 1609 lb |
| Vzletová hmotnost: Take-off Weight: | 1218 kg | 2685 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | ? kg | ? lb |
| Rozpětí: Wingspan: | 10,60 m | 34ft 9,31in |
| Délka: Length: | 7,90 m | 25ft 11,01in |
| Výška: Height: | 2,20 m | 7ft 2,6in |
| Plocha křídla: Wing Area: | 13,60 m2 | 146.39 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Lycoming O-435A o výkonu 142 kW/193 k dvoulistá vrtule | Lycoming O-435A, power 190 hp two-bladed propeller |
| Objem palivových nádrží: Fuel Tank Capacity: | ? | ? |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 275 km/h v ? m | 170.9 mph in ? ft |
| Cestovní rychlost: Cruise Speed: | 245 km/h v ? m | 152.2 mph in ? ft |
| Rychlost stoupání: Climb Rate: | 5,35 m/s | 1053.1 ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 6200 m | 20341 ft |
| Dolet: Range: | 1050 km | 652.4 mi |
| Maximální dolet: Maximum Range: | ? km | ? mi |
| Výzbroj: Armament: | - | - |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | - | - |
| Zdroje: Sources: | Andersson, Hanns G. Saab Aircraft since 1937. Smithsonian Institution Press, Washington 1989. ISBN 0-87474-314-1. Callaway, Tim. Light delight - the Saab 91 Safir, Aviation Classic Issue 16, 2012. Taylor, John W. R. All the World's Aircraft 1965-1966. Sampson Low, Marston & Co, London 1965. | |
SAAB 91B Safir
SAAB Sk 50B
http://commons.wikimedia.org/wiki/Category:Saab_91
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91B-2
Reklama
http://commons.wikimedia.org/wiki/Category:Saab_91
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Sk 50B
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F10 museum, Ängelholm, own photo
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