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The aluminum block Viking 110 has electronic ignition and multi-port fuel injection. It was introduced in 2009 and is based upon the 2009 model Honda Fit automotive engine. It produces 110 hp (82 kW) through a mechanical gear reduction drive with helical gears, with a reduction ratio of 2.33:1. A Warp Drive Inc propeller is recommended.
The Aircraft Bluebook Price Digest is a quarterly print publication by Informa (also available on CD-ROM) that was established in the 1950s. It identifies and prices more than 3,000 used general aviation aircraft and helicopter make and model-years available in the United States. Prices reflect historical data and cannot, therefore, take into ...
The earliest versions, developed in 1965, had a sea-level thrust of about 190 kN. By 1971, the thrust had improved to 540 kN, with resulting engine named Viking 1 and adopted for the Ariane program. The engine first flown on the Ariane 1 rocket in 1979 was Viking 2, with thrust further improved to 611 kN.
[17] [18] During 2008, Bombardier and Viking Air reached an arrangement under which the former sold the design documents and all intellectual property rights of all out-of-production de Havilland aircraft from the DHC-1 Chipmunk through the DASH-7 50 passenger STOL regional airliner to Viking. [19] [20] Its unit cost in 2014 was 36.9 million US ...
Developed by GE Aircraft Engines during the late 1960s, the original engine comprises a single stage fan, driven by a 4-stage low pressure (LP) turbine, supercharging a 14-stage high pressure (HP) compressor, driven by a 2-stage HP turbine. An annular combustor is featured.
The Savannah is a two-seat aircraft of conventional configuration and metal semi-monocoque construction. The high wing is braced to the fuselage by V-struts. Most variants have a constant-chord wing with combined flaperons. Initial models were fitted with full-span leading edge slots. The cabin seats two side by side under the wing.
The Dragonfly is a two-seater aircraft that features a tandem wing layout with a forward wing mounted low and the other behind the cockpit in a shoulder position, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed landing gear and a single engine in tractor configuration. The cockpit is 43 in (109 cm) wide [3]
An upgraded version of the engine has a chamber pressure of 58.5 bar as compared to 52.5 bar in the older version and produces a thrust of 800 kN. The engine is capable of gimballing. For launches from 2018 a 6% increased thrust version of the Vikas engine was developed. It was demonstrated on 29 March 2018 in the GSAT 6A launch second stage ...