| Název: Name: | Fisher P-75A | Fisher P-75A |
| Originální název: Original Name: | Fisher P-75A | |
| Kategorie: Category: | stíhací letoun | fighter aeroplane |
| Výrobce: Producer: | DD.MM.1944-DD.MM.194R Fisher Body Division, General Motors Corp., Cleveland, Ohio | |
| Období výroby: Production Period: | DD.MM.1944-DD.MM.194R | |
| Vyrobeno kusů: Number of Produced: | 5 P-75A, 1 nedokončený | |
| První vzlet: Maiden Flight: | DD.MM.RRRR | |
| 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: | 5120 kg | 11288 lb |
| Vzletová hmotnost: Take-off Weight: | ? kg | ? lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 8809 kg | 19420 lb |
| Rozpětí: Wingspan: | 15.04 m | 49ft 4in |
| Délka: Length: | 12.52 m | 41ft 1in |
| Výška: Height: | 5.03 m | 16ft 6in |
| Plocha křídla: Wing Area: | 32.24 m2 | 347 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 1 | |
| Typ: Type: | Allison V-3420-23 o výkonu 2151 kW Vrtule: trojlisté protiběžné | Allison V-3420-23, power 2885 hp three-blade contrarotating propellers |
| Objem palivových nádrží: Fuel Tank Capacity: | 2021 l | 534 US gal |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 693 1) km/h v ? m | 430.61) mph in ? ft |
| Cestovní rychlost: Cruise Speed: | ? km/h v ? m | ? mph in ? ft |
| Rychlost stoupání: Climb Rate: | 18,35 m/s | 3600 ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 11582 m | 38000 ft |
| Dolet: Range: | 3460.1 km | 2150 mi |
| Maximální dolet: Maximum Range: | 6196 km | 3850 mi |
| Výzbroj: Armament: | 10x pevný kulomet ráže 12,7 mm se zásobou 235/300 nábojů na hlaveň 2x puma o hmotnosti 227 kg | 10x .50 machine gun, 235/300 rpg 2x 500 lb bomb |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | Výkonové údaje jsou vypočteny, protože zkoušky nebyly oficiálně ukončeny 1) 644 km/hod skutečně dosažená | official performance trials were never completed 1) 404 mph real maximum speed |
| Zdroje: Sources: | http://joebaugher.com/usaf_fighters/p75.html www.nationalmuseum.af.mil www.military.cz http://www.airwar.ru/enc/fww2/p75.html aeroweb.brooklyn.cuny.edu http://www.aviastar.org/air/usa/fisher_p-75.php | |
Fisher P-75A
Photos of production P-75 Eagle
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Reklama
Three-view sketch of the P-75 Eagle
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This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.
L+K 3/1978, Letadla 1939-45, Václav Němeček
http://home.att.net/~jbaugher1/p75.html
www.nationalmuseum.af.mil
www.military.cz
http://www.airwar.ru/enc/fww2/p75.html
aeroweb.brooklyn.cuny.edu
http://www.aviastar.org/air/usa/fisher_p-75.php
archiv autora
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