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This page is an incomplete list of orbital rocket engine data and specifications. Current, upcoming, and in-development rocket engines Engine ... 200 (SL) 1,033,100 ...
The O-200 is an updated and upgraded version of the engine, achieving increased power of 100 hp (75 kW) as a result of higher maximum rpm. The standard and most common model of the engine is the O-200-A; the -B model is designed for a pusher installation, the -C model provides for the installation of a controllable-pitch propeller, and the -D ...
Falcon XR8 Sequential sedan : powered by a modified 5.0-Litre V8 engine producing over 200 kW (270 hp), its key feature was a Harrop-engineered and built sequential shift transmission; it also received a re-trimmed leather interior, upgraded brakes and suspension, 19-inch alloy wheels, twin bonnet air scoops and Mexican Fire paint that changed ...
GA-ASI's design is larger than the Sea Avenger and is powered by the Pratt & Whitney PW815 high-bypass turbofan, the same engine used on the Gulfstream G600. Generating 16,000 lb (7,300 kg) of thrust, it is four times more powerful than the Predator C's PW545B turbofan, [31] and the most powerful engine used by any Stingray competitor. [32]
The Franklin O-200 (company designation 4AC-199) was an American air-cooled aircraft engine of the early 1940s. The engine was of four-cylinder, horizontally-opposed layout and displaced 200 cu in (3 L). The power output ranged between 65 hp (48 kW) and 100 hp (75 kW) depending on variant. The O-200-5 (4ACG-199) featured a geared propeller drive.
The Rotax 914 is a turbo-charged, four-stroke, four-cylinder, horizontally opposed aircraft engine with air-cooled cylinders and water-cooled cylinder heads.It is designed and built by the Austrian company BRP-Powertrain, owned by Bombardier Recreational Products (BRP), as part of its Rotax brand.
The Continental O-190 (Company designations C75 and C85) is a series of engines made by Continental Motors beginning in the 1940s. Of flat-four configuration, the engines produced 75 hp (56 kW) or 85 hp (63 kW) respectively. [1] The two variants shared the same bore, stroke and compression ratio.
Data from Jane's All the World's Aircraft 1982–83 General characteristics Crew: 1 pilot Capacity: 1 passenger Length: 18 ft 0 in (5.49 m) Wingspan: 25 ft 0 in (7.62 m) Height: 8 ft 0 in (2.44 m) Wing area: 105.0 sq ft (9.75 m 2) Empty weight: 733 lb (332 kg) Max takeoff weight: 1,270 lb (576 kg) Fuel capacity: 23 US gal (19 imp gal; 87 L) Powerplant: 1 × Continental O-200 -A air-cooled flat ...