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The aircraft was initially fitted with a bubble canopy. Later, the fuselage was modified to allow a more reclined pilot seating position and the canopy replaced with a more streamlined one. The modifications added 200 lb (91 kg) to the glider's empty weight and the gross weight was raised 100 lb (45 kg) in partial compensation.
The design was by Dipl-Ing Klaus Holighaus and the prototype first flew in May 1974. The production examples incorporated several improvements in January 1975. The Janus has a glass-fibre monocoque fuselage similar to that of the Nimbus-2 but the cockpit section is lengthened to accommodate the two pilots in tandem with dual controls under a right-hand side-hinged one-piece canopy.
The SZD-49 Jantar K was a 15m Class glider designed and built in Poland ... A one-piece forward-opening canopy with integral glare-shield gave access to the cockpit ...
The aircraft then becomes a pure glider, with a best glide ratio of around 1:28. The Porsche-derived horizontally opposed air-cooled engine had the cylinder bore increase by Grob to make the engine 2.5-litre capacity and has had its Time Before Overhaul (TBO) increased by a technote to 1,600 hours after many examples run on condition reached up ...
Kortenbach & Rauh Kora 1973 Motor glider, 2 built; Lartin Skylark 1973 Utility Prototype; PZL M-17 1973 Trainer Prototype; Edgley Optica 1979 ducted fan observation aircraft 21 built; 1980 and later ADI Condor 1981 2 seat motorglider, unk no. built; Acapella 200 1982 homebuilt, 1 built [6] Applebay Zia 1982 1 seat ultralight motorglider, 4 built
Both have a simple, deep, sprung landing skid reaching from the nose to under the trailing edge of the wing, assisted by a tail bumper. Their cockpits are under the wing leading edge, into which the clear canopy extends. [1] The Ka 1 first flew in 1951 and ten were built; [2] the Ka 3 followed in 1954 with fifteen eventually completed. [1]