| Název: Name: | Lockheed P2V-1 Neptune | Lockheed P2V-1 Neptune |
| Originální název: Original Name: | Lockheed P2V-1 Neptune | |
| Kategorie: Category: | protiponorkový/protilodní letoun | aeroplane for anti-submarine/anti-ship warfare |
| Výrobce: Producer: | DD.09.1946-DD.03.1947 Lockheed Aircraft Corp., Burbank, California | |
| Období výroby: Production Period: | DD.09.1946-DD.03.1947 | |
| Vyrobeno kusů: Number of Produced: | 14 (89082/89085, 89087/89096) | |
| První vzlet: Maiden Flight: | 17.05.1945 XP2V-1 | |
| Osádka: Crew: | 8 | |
| 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: | 15295 kg | 33720 lb |
| Vzletová hmotnost: Take-off Weight: | 20412 kg | 45000 lb |
| Maximální vzletová hmotnost: Maximum Take-off Weight: | 27739 kg | 61153 lb |
| Rozpětí: Wingspan: | 30.48 m | 100ft |
| Délka: Length: | 23.01 m | 75ft 6in |
| Výška: Height: | 8.56 m | 28ft 1in |
| Plocha křídla: Wing Area: | 92.9 m2 | 1000 ft2 |
| Plošné zatížení: Wing Loading: | ? kg/m2 | ? lb/ft2 |
| Pohon: Propulsion: | ||
| Kategorie: Category: | pístový | piston |
| Počet motorů: Number of Engines: | 2 | |
| Typ: Type: | Wright R-3350-8A o vzletovém výkonu 1715 kW čtyřlistá vrtule s konstantní rychlostí otáček Hamilton Standard | Wright R-3350-8A, take-off power 2300 hp four-bladed constant-speed propeller Hamilton Standard |
| Objem palivových nádrží: Fuel Tank Capacity: | 12681 l | 3350 US gal |
| Výkony: Performance: | ||
| Maximální rychlost: Maximum Speed: | 487.6 km/h v 4663 m | 303 mph in 15300 ft |
| Cestovní rychlost: Cruise Speed: | 283.2 km/h v 457 m | 176 mph in 1500 ft |
| Rychlost stoupání: Climb Rate: | 5.3 m/s | 1050 ft/min |
| Čas výstupu na výšku: Time to Climb to: | ? min do ? m | ? min to ? ft |
| Operační dostup: Service Ceiling: | 8230 m | 27000 ft |
| Dolet: Range: | ? km | ? mi |
| Maximální dolet: Maximum Range: | 6646.6 km | 4130 mi |
| Výzbroj: Armament: | 2x kulomet Browning ráže 12,7 mm v přídi 2x kulomet Browning ráže 12,7 mm ve hřbetní věži Martin 250CE 2x kulomet Browning ráže 12,7 mm v ocasní věži Bell 3629 kg bomb nebo torpéd 16x raketa HVAR nebo 4x raketa Tiny Tim | 2x .50 in Browning machine gun in the nose 2x .50 in Browning machine gun in the Martin 250CE dorsal turret 2x .50 in Browning machine gun in the Bell rear turret 8000 lb of bombs or torpedoes 16x HVAR rocket or 4x Tiny Tim rocket |
| Uživatelské státy: User States: | | |
| Poznámka: Note: | - | - |
| Zdroje: Sources: | Sullivan, Jim. P2V Neptune in action, No.68. Squadron/Signal Publications, Carrollton 1985. ISBN 978-0-89747-160-2. Anderson, Holmes G. The Lockheed P2V neptune, profile No.204. Profile Publications, Leatherhead 1967. Francillon, René J. Lockheed Aircraft since 1913. Naval Institute Press, Annapolis 1987. ISBN 0-85177-835-6. Munson, Kenneth. Bombers in service: Patrol and Transport Aircraft since 1960. Blandford Press, 1978. ISBN 0-7137-0744-5. Swanborough, G., Bowers, P. M. United States Navy Aircraft since 1911. Putnam Aeronautical Books, London 1990, ISBN 0-85177-838-0. | |
Lockheed P2V-1 Neptune
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XP2V-1
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P2V-1
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| Type | Lockheed P2V-1 Neptune |
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