The ESG Grunau 9, later known as the ESG 29 and post-1933 as the DFS 108-10, was one of the first primary gliders, built in Germany from the late 1920s. It was widely sold. Design and development The Grunau 9 was a German single seat trainer glider, one of the first of a group that later became known as primary gliders. It was developed by Edmund Schneider from Alexander Lippisch's Djävlar Anamma (, ) via the Espenlaub primary. The Grunau 9 was produced in numbers and was sold widely. The core of the flat frame fuselage was formed with a horizontal beam about long, to which two other converging struts were attached, making overall a vertical A-frame. The downward sloping extremities of these beams carried a slightly deeper horizontal box structure below the cross beam, with the open pilot's seat and controls upon it. On some later aircraft there was an extra vertical member for the lower cross beam to the wing root to provide the pilot with a backrest. Others enclosed him or her in a simple, light, short nacelle between the nose and the backrest strut. The rear part of the fuselage frame was based on two longer beams reaching to the tail. The upper one was horizontal and attached to both converging A-frame beams, near but not at its apex. The lower one sloped upwards and was attached to the rear sloping part of the A-frame just below the cross-member. These two rear fuselage beams were cross braced with three more struts, one vertical about halfway to the tail, forming two bays which were crossed diagonally by the other two struts. There was another, short vertical strut in the rear bay between the upper and diagonal members. For landings a skid ran between three projecting ends of the forward and lower A-frame. The Grunau 9 had almost rectangular, two spar, wooden structured, two piece wings with fabric covering everywhere except the leading edges, which were plywood covered. Short, simple rectangular, cropped ailerons reached to the square wing tips. They were attached to the upper fuselage beam with their leading edges at the forward sloping member and a chordwise gap between their roots. Each wing was braced with a pair of landing wires from the apex of the A-frame to the upper wing at outboard points on the forward and aft spars and by pairs of flying wires