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The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. [3]The original 60 kW (80 hp) 912 UL engine has a capacity of 1,211 cc (73.9 cu in) and a compression ratio of 9.1:1, and is designed to work with regular automotive gasoline, with up to 10% ethanol.
The RV-12iS is an incremental improvement over the RV-12 which allows the installation of the Rotax 912ULS (carbureted) or the Rotax 912iS (fuel-injected) engines. It also incorporates a new cowling and throttle quadrant design, quick-retracting flaps, a quick-adjusting seat, redesigned landing gear attachments and fuel tank, among other ...
Development of the Sling 2 commenced in 2006. The Sling is a two-seat, low wing, all metal aircraft with tricycle landing gear made from composites. The aircraft is powered by an 80 hp (60 kW) Rotax 912UL,100 hp (75 kW), a Rotax 912ULS, or a 912iS engine, or optionally a turbocharged 115 hp (86 kW) Rotax 914 UL, driving a 3-bladed Warp Drive Inc propeller.
The Rotax 915 iS is an Austrian aircraft engine, produced by Rotax of Gunskirchen for use in ultralight aircraft, homebuilt aircraft, light-sport aircraft, small helicopters and gyroplanes. The engine was type certified in 2017. [2] [3] The engine was first publicly displayed at AirVenture in July 2015 [2] and first flown in March 2016. [4]
Rotax is the brand name for a range of internal combustion engines developed and manufactured by the Austrian company BRP-Rotax GmbH & Co KG [1] (until 2016 BRP-Powertrain GmbH & Co. KG), in turn owned by the Canadian Bombardier Recreational Products (BRP). Under the Rotax brand, the company is one of the world's largest producers of light ...
EASA type-certified model in the CS-LSA category. Short wing version powered by a 100 hp (75 kW) Rotax 912 S3 engine. [11] Virus SW 600 D Based on the SW 121 but featuring a 100 hp (75 kW) Rotax 912 ULS engine, it is the first aircraft to be certified under the new German LTF-UL2019 rules for the 600 kg microlight category. [22]
Rotax 912; Metadata. This file contains additional information, probably added from the digital camera or scanner used to create or digitize it.
The cockpit width is 1.15 m (45 in). Standard engines available are the 100 hp (75 kW) Rotax 912ULS, the Rotax 912iS [5] and the 115 hp (86 kW) Rotax 914 four-stroke powerplants. A glider towhook is optional equipment. [2] [3] [6] The design has been developed into a three to four seat aircraft, the Aerospool WT10 Advantic. [2]