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The Nimbus-4DM is a model of the "Nimbus-4 Family," which consists of single-seat and two-seat gliders and motor gliders. The engine in each motor glider retracts into the fuselage, behind the cockpit. The different models are (production data as of 1999): Nimbus-4: a single-seat glider, type certified in Germany January 1, 1994.
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.
LS1-f - introduced the one-piece canopy, conventional tailplane, redesigned rudder and structural changes that allowed more water ballast and higher flight mass. It also has a reduced wing incidence relative to the fuselage, resulting in noticeably better high speed performance than the earlier LS1 variants.
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
It is a Standard Class glider with a 15-metre span, and laminar-flow airfoil section designed by Professor Franz Wortmann. The all-moving tailplane, a feature of many designs of that period due to its theoretically higher efficiency, caused less than desirable high-speed stability characteristics, and so modifications were made to the early design.