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principal motor Power output Image 4-8+8-4-750/8-DE: 1943: 1: 2-D-D-2: 408 (×8) 6,000 hp (4.47 MW) (only 4 of the 8 engines actually installed) 0-6-6-0 1000/1 DE: 1945 30 for Soviet Railroads C-C 1,000 hp (750 kW) DR-12-8-1500/2 "Centipede" 1945–1948: 56: 2-D-D-2: 608SC (×2) 3,000 hp (2.24 MW) DR-6-4-2000: 1945: 2: A1A-A1A: 8-VO (×2) 2,000 ...
The ultimate British 0-6-0 was the Q1 Austerity type, developed by the Southern Railway during the Second World War to haul very heavy freight trains. It was the most powerful steam 0-6-0 design produced in Europe. Similarly, the 0-6-0 tank locomotives became the most common locomotive type on all railways throughout the 20th
The Baldwin 0-6-6-0-1000/1DE is a cab unit diesel-electric locomotive built by Baldwin Locomotive Works in 1945. The 0-6-6-0-1000/1DEs were powered by an eight-cylinder diesel engine rated at 1,000 horsepower (746 kW), and rode on a pair of three-axle trucks in a C-C wheel arrangement. 30 of these models were built for Soviet Railways, today Russian Railways, as Class Д б (Class Db).
Between 1913 and 1926, Belgian locomotive builders Société Anonyme St. Leonard of Liège constructed 31 Garratt 0-6-0+0-6-0 locomotives for the 750 mm (2 ft 5 + 1 ⁄ 2 in) gauge Compagnie du C.F. du Congo in the Belgian Congo. The locomotives were delivered in four batches, one in 1913, twelve in 1920-21, eight in 1924-25 and the last ten in ...
Initially, the "K" type engine developed in the 1930s were offered in I4, I6, I7 and I8 variants, had 2-valve cylinder heads and ran at 600-680rpm. In 1940, turbocharging became an option, boosting power output by about 61%.
As realized in the 2007 Volt concept, the initial E-Flex design includes an electric traction motor with peak power and torque outputs of 120 kW (160 hp) and 320 N⋅m (240 lbf⋅ft), a 1 L 3-cylinder gasoline engine coupled to a generator with an output of 53 kW (71 hp), and a 16 kWh (58 MJ) lithium-ion battery energy storage system.
Rutherford is a liquid-propellant rocket engine designed by aerospace company Rocket Lab [8] and manufactured in Long Beach, California. [9] The engine is used on the company's own rocket, Electron. It uses LOX (liquid oxygen) and RP-1 (refined kerosene) as its propellants and is the first flight-ready engine to use the electric-pump-fed cycle.
The Tipo F163 BC is a 3.0 L, 120°, twin-turbo V6 engine; that has a maximum output of 663 PS (654 hp; 488 kW) at 8,000 rpm, in combination with a 167 PS (165 hp; 123 kW) electric motor. The electric motor complements 232 lb⋅ft (315 N⋅m); bringing the total combined system output to 830 PS (819 hp; 610 kW) and 546 lb⋅ft (740 N⋅m).
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