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In designing the Mini-Nimbus, Klaus Holighaus incorporated the flapped wings from the Glasflügel 303 Mosquito, with the fuselage of the Standard Cirrus. The wings feature trailing edge terminal speed dive brakes-variable camber flaps that limit the vertical dive speed to a maximum of 70 knots when the dive brakes are fully deployed [citation needed].
The Schempp-Hirth Cirrus is an Open Class glider built by Schempp-Hirth between 1967 and 1971 and by VTC until 1977. It was replaced by the Nimbus 2. Development
The Standard Cirrus is a Standard-class glider built in Germany by Schempp-Hirth. The Standard Cirrus was produced between 1969 and 1985, when it was replaced by the Discus . Over 800 examples were built, making it one of the most successful early fibreglass glider designs.
Cirrus Design VK-30 on ramp at the Baraboo–Wisconsin Dells Airport in Baraboo, Wisconsin, c. 1988. The VK-30 design was conceived in the early 1980s as a kit plane project by three Wisconsin college students: Alan Klapmeier and Jeff Viken from Ripon College, and Alan's brother, Dale Klapmeier, who was attending the University of Wisconsin–Stevens Point.
The Cirrus SR22 is a single-engine four- or five-seat composite aircraft built since 2001 by Cirrus Aircraft of Duluth, Minnesota, United States.. It is a development of the Cirrus SR20, with a larger wing, higher fuel capacity and more powerful, 310-horsepower (231 kW) engine, and a 315 hp (235 kW) engine for the turbocharged version of the aircraft.
Photo series showing a Cirrus SR20 deploying the Cirrus Airframe Parachute System (CAPS) during inflight testing in 1998. The Cirrus Airframe Parachute System (CAPS) is a whole-plane ballistic parachute recovery system designed specifically for Cirrus Aircraft's line of general aviation light aircraft including the SR20, SR22 and SF50.
The Cirrus Vision SF50, also known as the Vision Jet, is a single-engine very light jet designed and produced by Cirrus Aircraft of Duluth, Minnesota, United States. After receiving deposits starting in 2006, Cirrus unveiled an aircraft mock-up on 28 June 2007 and a prototype on 26 June 2008.
Data from Cirrus SR20 Specifications Webpage General characteristics Crew: 1 Capacity: 3 Length: 26 ft 0 in (7.92 m) Wingspan: 38 ft 4 in (11.68 m) Height: 8 ft 11 in (2.72 m) Empty weight: 2,126 lb (964 kg) Gross weight: 3,050 lb (1,383 kg) Powerplant: 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine, 200 hp (150 kW) Propellers: 3-bladed Performance Cruise ...
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