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The engine weighed 130 lb (59 kg) which was slightly heavier than the 750 engine but 31 lb (14 kg) lighter than the engine of the GSX1300R. The performance of the engine is a peak of 160 bhp (119 kW) at 9,500 rpm, as measured on the crank and 143 hp (107 kW), [2] when measured on the rear wheel with small variations between different instances ...
Merit (UK) - ceased production of plastic model aircraft sometime in the late 1950s; Merit International (USA) Merlin Model (UK) MGD Models (Czech Republic) Micro Ace (Japan) - ex-Arii; Micro Scale Design (Russia) Midori Plastic. Kit (KSN) (Japan) Mikro72 (Poland) MikroMir (Ukraine) MiniArt (Ukraine) Minibace (China) Minicraft Model Kits, Inc ...
Two seats in tandem model with dual controls and a 24 ft (7.3 m) wingspan. Standard engine is the 50 hp (37 kW) Rotax 503 and the acceptable power range is 40 to 80 hp (30 to 60 kW). The 64 hp (48 kW) Rotax 582 and 75 hp (56 kW) Rotax 618 two-stroke engines were optional. It was available as a kit or ready-to-fly and production is completed.
Produced by Volvo Aero, the RM12 is a derivative of the General Electric F404J. The fan was completely redesigned with thickened first stage blades which deform (causing the thrust loss) but do not fracture or cause downstream damage to pass more flow for higher thrust and to be more tolerant of a bird-strike.
The first GSX-R of 1984 was a breakthrough model and the closest that any Japanese manufacturer had yet come to building a "race bike with lights". Throughout the 1970s the big four Japanese manufacturers had built bikes with a similar architecture: steel double loop frames, air-cooled transverse fours with either SOHC or DOHC configurations.
The aircraft replaces the Spyder's two-stroke engine with a Yuneec Power Drive 20 20 kW (27 hp) electric motor and two 28 lb (13 kg) Lithium polymer battery packs which provide a 40-minute endurance. The aircraft is intended to be developed into a commercially available kit and forecast to be available for under US$25,000.
When the GSX-R entered development, Suzuki set a goal of 100 horsepower (75 kW) for a 750 engine and, due to known heat-related problems in high-power air-cooled engines, determined that air cooling alone would not be sufficient. Therefore, the SACS system was applied to the bike's design and was eventually carried over to all larger GSX-Rs.
The American Federal Aviation Administration certified the engine for commercial operation on January 4, 2006. [4] The engine was ground run for the first time on an A380 on August 14, 2006, in Toulouse. [5] On August 25, 2006, the same aircraft, A380-861 test aircraft (MSN 009), made the first flight of an Engine Alliance powered A380.