EKW C-36 - Снимки и видео

ЕКВ С-36
Страна	Швейцария
Роля	Наземни самолети
Първи полет	15 май 1939 г.
Построен	175

1. ЕКВ С-36 е швейцарски многоцелеви боен самолет от 30-те и 40-те години на миналия век, построен от Eidgenoessische Konstruktionswerkstaette. Това беше едномоторен моноплан с екипаж от двама. Той влиза в експлоатация по време на Втората световна война през 1942 г. и въпреки че е остарял, остава в употреба на фронтовата линия до началото на 50-те години и като целеви влекач до 1987 г.

Източник: EKW C-36 в Уикипедия

EKW C-36 Walk Around
Фотограф	Ales Pavias
Локализация	Не знам
Снимки	16

Copie de EKW C-36 2

Copie de EKW C-36 1

Copie de EKW C-36 4

Copie de EKW C-36 3

Copie de EKW C-36 6

Copie de EKW C-36 5

Copie de EKW C-36 8

Copie de EKW C-36 7

Copie de EKW C-36 9

Click on a photo and use the mouse scroll to view all photos

Изчакайте, Търсене EKW C-36 снимки за вас...

General Characteristics (C-3603 Production Variant)

The EKW C-36 was a Swiss-designed and built multi-purpose combat aircraft developed in the late 1930s and used throughout World War II and the early Cold War. Designed by the Eidgenössische Konstruktionswerkstätte (EKW), it served primarily as a reconnaissance, ground attack, and fighter-bomber for the Swiss Air Force, defending the nation’s neutrality. It is known for its twin-boom tail and long career, later serving as a target tug until 1987 in the turboprop C-3605 variant.

Property	Typical Value (C-3603)
Роля	Reconnaissance / Ground Attack / Target Tug
Производителя	EKW (Eidgenössische Konstruktionswerkstätte)
First Flight	May 15, 1939 (C-3601 Prototype)
Екипажа	2 (Pilot and Observer/Rear Gunner)
Дължина	10.23 m (33 ft 7 in)
Размах	13.74 m (45 ft 1 in)
Max Takeoff Weight	3,952 kg (8,713 lb)

Design and Powerplant

Engine: One Hispano-Suiza 12Y-51 V-12 liquid-cooled piston engine (built under license).
Power Output: 746 kW (1,000 hp).
Design Features: All-metal low-wing cantilever monoplane. It featured a distinctive twin-boom tail (twin vertical stabilizers) to give the rear gunner an unobstructed field of fire.
Landing Gear: Retractable undercarriage was introduced on the production C-3603 variant (prototypes had fixed gear).
Later Variant (C-3605): A number of C-3603 airframes were converted into the C-3605 turboprop target tug, fitted with a Lycoming T53 engine and an extended nose, earning it the nickname “Alpine Anteater” or “Flying Zebra Crossing.”

Performance and Armament

Maximum Speed: Up to 476 km/h (296 mph, 257 knots) at altitude.
Service Ceiling: 8,700 m (28,550 ft).
Range: Approximately 680 km (425 mi, 369 nmi).
Rate of Climb: 10.4 m/s (2,050 ft/min).
Armament (C-3603):
- Forward: One 20 mm Oerlikon cannon firing through the propeller hub.
- Wings: Two 7.5 mm machine guns in the wings.
- Rear: Two 7.5 mm machine guns in a flexible mount for the rear gunner.
- Ordnance: Up to 400 kg of bombs carried under the wings and fuselage.
Armament (C-3604): An improved version with a Saurer YS-2 engine and two extra 20 mm cannons in the wings.