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The prototype was a two-cylinder model capable of 80 hp (60 kW). The three-cylinder WAM120 produced 100–120 hp (75–89 kW), and the factory intended to produce a follow-up four-cylinder 160 hp (119 kW) motor to compete with engines such as the Lycoming O-360. However, funding proved problematic, and it became expedient to extend the product ...
The Firewall Forward CAM 100 is a 100 hp (75 kW) four-cylinder, four-stroke liquid-cooled piston aircraft engine built by Firewall Forward Aero Engines. [1] Originally designed and built by Canadian Airmotive as the CAM 100 and later marketed by The Cam-Fire Engine Group, [2] it is based on a Honda Civic automotive piston engine.
The Rapp 100 hp was a four-cylinder, SOHC valvetrain liquid-cooled inline aircraft engine built by Rapp Motorenwerke.The engine originated from Karl Rapp's earlier 90 hp four-cylinder that he had designed at the Flugwerk Deutschland GmbH for the 1912/13 Kaiserpreis aircraft engine contest.
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 ...
The Dair 100 engine is a twin-cylinder two-stroke, opposed-piston, 1,810 cc (110.5 cu in) displacement, liquid-cooled, diesel engine direct drive design. It produces 100 hp (75 kW) at 2500 rpm, with a compression ratio of 18:1. [1]
It was designed to output around 1800 hp (1340 kW), or 100 hp (75 kW) per cylinder. However, the tight design of the engine made it difficult to maintain quality in manufacturing, and unreliability in the field was a significant problem; actual output of early models at altitude was in the range of 1300 hp (970 kW), far below the designed ...
The LMS100 comprises a low-pressure compressor, an intercooler, a supercore and a power turbine. The supercore (comprising a HP compressor, compressor rear frame, high-pressure turbine and intermediate pressure turbine) is a further development of the LM6000, which in turn was based on the CF6-80C2. The low-pressure compressor is from the 6FA ...
Improved model, with higher gross weight, powered by an 80 hp (60 kW) Rotax 912UL four-stroke powerplant and introduced in 1992 by Aero Designs. [2] Pulsar Series II Improved model, powered by a 100 hp (75 kW) Rotax 912ULS four-stroke or 115 hp (86 kW) Rotax 914 turbocharged powerplant and produced by SkyStar Aircraft. Pulsar III