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The SGS 1-26 enjoyed a very long production run from its first flight in 1954 until 1979, when production was ended. The 1-26 was replaced in production by the Schweizer SGS 1-36 Sprite. The 1-26 is the most numerous sailplane found in the US. [1] [4] In October 1963 a special issue of Soaring magazine was dedicated to the 1-26. Harner Selvidge ...
Schweizer SGS 1-23D sailplane. The 1-23 was first flown in 1948. The Schweizer SGS 1-23 was a world class competition and record setting glider between its first flight in 1948 and the end of its production in 1967. [9] In the 1950s and 1960s the Schweizer Aircraft Corporation designed and manufactured the very popular SGS 1-26 and SGS 2-33 gliders
United States sailplanes by decade of first flight 1910s • 1920s • 1930s • 1940s • 1950s • 1960s • 1970s • 1980s • 1990s • 2000s • 2010s • 2020s
X-26 glider circa 1983 Two Schweizer 2-32s, 67-15345 and 67-15346, from the U.S. Naval Test Pilot School X-26 Program, were modified to QT-2 configuration (QT for Quiet Thruster) by the Lockheed Missiles & Space Company and civil registered as N2471W and N2472W.
In March 1961, Scott took his first flight in a glider and within a few months he had purchased a new Schweizer SGS 1-26 sailplane. [ 12 ] Scott’s first record flight was an 8.5 hour, 443.5 mi (714 km), dog-leg flight from Odessa, Texas to Clayton, New Mexico flown on August 6, 1963. [ 13 ]
SZD-50-1 Dromader The initial design and prototype of the Puchacz series, first flown on 21 December 1976; two built. SZD-50-2 Puchacz Initial production variant first flown on 13 April 1979. SZD-50-3 Puchacz Later production standard with fin mounted 300 mm (12 in) higher, enlarged rudder and main-wheel fairing.
Data from British Gliders and Sailplanes 1922-1970, [1] Slingsby Sailplanes, [2] and The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde [3] General characteristics. Crew: 1; Length: 20 ft 11 in (6.38 m) Wingspan: 45 ft 0 in (13.72 m) Wing area: 113 sq ft (10.5 m 2) Aspect ratio: 17.9
[1] [2] It is a shoulder wing competition sailplane. The first aircraft, the Phoebus A, was designed to Standard Class rules, with a span of 15 m. Its straight tapered wings have an aspect ratio of 17.1; airbrakes are fitted at 70% chord. The fin and rudder are straight edged and only slightly tapered, with a high aspect ratio all moving T tail.