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The F7 was powered by a 7.0 L LS7 V8 engine, which had a capacity of 7 liters and a power of 629 HP, transferring power to the rear axle in cooperation with a 6-speed manual transmission. The car reached 0–60 mph (0–97 km/h) in 3.3 seconds, and the maximum speed was about 200 mph (320 km/h).
In 2012, Falcon presented the production version of the Falcon F7 to the international automotive press. This was the company's inaugural vehicle. [7] The F7 is a mid engine rear-wheel-drive two seat sports car with a monocoque chassis built from aluminum, carbon fiber and Kevlar.
The 567B engine was uprated to 1,500 hp (1.1 MW). Some F3s were nicknamed "chickenwire" for the type of engine room air-intake structure along the sides. The F7 (1949) and F9 (1954) were evolutionary: the F7 had improved traction motors, the F9 a 1,750 hp (1.30 MW) 567C engine. A louver arrangement over the vents changed their appearance from ...
The CFE CFE738 is a small turbofan engine aimed at the business/commuter jet market ... The CFE738-1 made its inaugural flight on a Falcon 2000 prototype on March 4 ...
The Ford Falcon is a full-size car that was manufactured by Ford Australia from 1960 to 2016. From the XA series of 1972 onward, each Falcon and range of derivates have been designed, developed, and built in Australia, following the phasing out of the American-influenced Falcon of 1960 to 1971, which had been re-engineered locally as the XK to XY series for the harsher Australian conditions.
Falcon 300+ coupé: unveiled at the 2001 Melbourne Motor Show, this car was produced by Advanced Engine Components (AEC) and Miller Design at a cost of A$1 million, with production aspirations originally supported by Ford Australia's Geoff Polites; it was fitted with a Fairmont interior and a supercharged Ford Mustang-sourced 4.6-litre engine ...
Rocket engines [14] Armstrong Siddeley Alpha; Armstrong Siddeley Beta; Armstrong Siddeley Delta; Armstrong Siddeley Gamma; Armstrong Siddeley Screamer; Armstrong ...
Each Falcon 9 booster uses nine Merlin engines, and the second stage uses one Merlin vacuum engine. The second stage is expended, so each launch consumes one Merlin Vacuum engine. SpaceX designed the booster with its engines to be recovered for reuse by propulsive landing, and the first recovered booster was reused in March 2017.