Description
Intended for pleasure flying rather than contests or competitions, the BJ-1 Duster single-seater is specifically designed for homebuilt construction from plans. No component of the simple wooden structure exceeds 18ft in length so that it can be built at home and in the garage; the average construction time is approximately 600-700 hours.
Designed by Ben Jansson, an aerodynamicist who captained the Swedish teams in the 1968 and 1970 World Gliding Championships, and H.Einar Thor, the Duster is marketed by the DSK Aircraft Corporation of Van Nuys, California.
Design work began in early 1964 and the prototype BJ-1 first few in August 1966. The cantilever shoulder wing is built in three pieces – a 7ft span centre-section integral with the fuselage and two outer panels – and there is a single spruce main spar with plywood ribs and covering. The trailing edge flaps also act as air brakes. The straight-sided fir plywood fuselage has an elongated hexagonal cross-section in the cockpit area changing to a triangular cross-section aft of the wings. There is a ventral plywood keel reinforced by two bulkheads shaped to the seat contour and supporting a floor-mounted seat. There is a nonretractable semi-recessed monowheel beneath the keel, as well as a tailwheel; the fuselage nose cone and fairings are of glassfibre. The tailplane is mounted on top of the fuselage and the tail unit is of similar construction to the wings, all tail surfaces being plywood-covered.
The BJ-lb differs from the BJ-1 in having a slightly increased wing span, a reduced weight and a Plexiglas canopy reduced in height to allow the pilot to sit in a semi-reclining position; it can be flown with this one-piece flushfitting canopy or with an open cockpit and just a windscreen.
An auxiliary power package for the Duster was under development in 1977 using a 26hp engine mounted dorsally, and the plans provided give details of all the changes necessary to support an engine mounting, which can then be added when the builder so desires without further alteration of the airframe. Previously, a version of the BJ-1b powered by a 35hp Rockwell JLO-600LM ‘flat twin’ engine mounted behind the cockpit on struts and driving a two-blade fixed-pitch wooden pusher propeller was flown in 1973. This powered version was produced by the Duster’s co-designers, Hank Thor and Ben Jansson, and the engine is not retractable into the fuselage.
Approximately 400 sets of plans and 150 component kits have been sold to homebuilders. In accordance with former OSTIV rules it has terminal-velocity-limiting dive brakes (216 kph/ 116 kt./ 134 mph. The Duster has been built in Canada and 10 other countries, and is type-certified in New Zealand. It is relatively simple to build but the 2.13 m/ 7 ft fixed center section provides a challenge for trailer design.
BJ-1 Duster
Wing span: 13.0 m (42 ft 7 in)
Length: 6.1 m (20 ft 0 in)
Wing area: 9.60 sq.m (103.3 sq ft)
Wing section: NACA 4415
Aspect ratio: 17.7
Empty weight: 159 kg (350 lb)
Max weight: 263 kg (580 lb)
Water ballast: None
Max wing loading: 27.4 kg/m 2 (5.61 lb/sq ft)
Max speed: 111 kt (206 km/h)
Stalling speed: 34.5 kt (64 km/h)
Min sinking speed at 67 kt (124 km/h): 1.8 m (5.9 ft)/sec
Max rough air speed: 80 kt (148 km/h)
Best glide ratio at 47 kt (87 km/h): 29
