| Název: Name: | North American YF-107A | North American YF-107A |
| Originální název: Original Name: | North American YF-107A | |
| Kategorie: Category: | stíhací letoun | fighter aeroplane |
| Výrobce: Producer: | DD.08.1956-DD.MM.1956 North American Aviation, Inc., Inglewood, California | |
| Období výroby: Production Period: | DD.08.1956-DD.MM.1956 | |
| Vyrobeno kusů: Number of Produced: | 3 (55-5118/5120) | |
| První vzlet: Maiden Flight: | 10.09.1956 | |
| Osádka: Crew: | 1 | |
| 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: | 11405 kg | 25144 lb |
| Vzletová hmotnost: Take-off Weight: | 18033 kg | 39755 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 18841 kg | 41537 lb |
| Rozpětí: Wingspan: | 11.15 m | 36ft 7in |
| Délka: Length: | 18.54 m | 60ft 10in |
| Výška: Height: | 5.99 m | 19ft 8in |
| Plocha křídla: Wing Area: | 34.1 m2 | 367,02 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | jednoproudový | turbojet |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Pratt & Whitney YJ75-P-9 o tahu 76,50 kN / 108,98 kN s přídavným spalovaním | Pratt & Whitney YJ75-P-9, thrust 17200 lb.st. / 24500 lb.st. with afterburner |
| Objem palivových nádrží: Fuel Tank Capacity: | 4770 l 1893 l nádrž pod trupem | 1260 US gal 500 gal belly tank |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 2084.1 km/h v 10973 m | 1295 mph in 36000 ft |
| Cestovní rychlost: Cruise Speed: | 946.3 km/h v ? m | 588 mph in ? ft |
| Rychlost stoupání: Climb Rate: | 202.7 m/s | 39900 ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 16215 m | 53200 ft |
| Dolet: Range: | 1268.2 km | 788 mi |
| Maximální dolet: Maximum Range: | 3907.5 km | 2428 mi |
| Výzbroj: Armament: | 4x 20 mm kanon M39, 200 nábojů každý 4536 kg podvěšené výzbroje | 4x 20 mm M39 cannon, 200 rpg 10000 lb of ordnance |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | - | - |
| Zdroje: Sources: | Davies, Peter E.; Menard, David W. North American F-100 Super Sabre. Crowood Press, Ramsbury 2003. ISBN 1-86126-577-8. http://joebaugher.com/usaf_fighters/f100_4.html www.nationalmuseum.af.mil | |
North American YF-107A
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North American YF-107A pilotny priestor
Reklama
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North American YF-107A
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North American YF-107A
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