Bréguet Br 900 Louisette

Bréguet Br 900 Louisette
Role	Single seat competition sailplane
National origin	France
Manufacturer	Société des Ateliers d'Aviation Louis Bréguet (Breguet Aviation)
Designer	Georges Ricard
First flight	17 June 1948
Number built	8

The Bréguet Br 900 Louisette is a short span, single seat competition sailplane built in France in the 1940s. It set some French gliding records but was unsuccessful at the international level. Only six production aircraft were built.

Design and development

Despite its long history of aircraft design and production, Bréguet Aviation had not built a glider before the 900. After World War II they found themselves with many craftsmen who had skills in building with wood, so light aviation and unpowered aircraft offered a market opportunity. George Ricard designed a wooden, single seat, mid-wing cantilever monoplane which, though intended for competition, had the comparatively short span of 14.35 m (47 ft 1 in).

The wings of the Bréguet 900 are straight tapered, with squared off tips with small tip fences. They have marked dihedral. Forward of the single box spar the wing is plywood covered, with fabric aft. Narrow ailerons occupy the outer halves of the wing trailing edge, with flaps of the same chord inboard. From the second prototype onwards the Bréguet 900 has had spoilers at about mid-chored just inboard of the ailerons. On the earliest aircraft these were of the DFS type but were later replaced by Schempp-Hirth parallel ruler action brakes.

The fuselage of the Bréguet 900 is plywood covered and of oval cross-section, near circular aft of the wing and deepening markedly to accommodate the cockpit. Fin and rudder are also ply covered, bearing fabric covered control surfaces. The horn balanced rudder is broad and reaches between the elevators to the bottom of the fuselage. Some production aircraft had taller vertical surfaces than those of earlier 900s. The straight tapered horizontal surfaces fold upwards for ease of transport. Early models used an angular, multi-piece canopy, later supplanted by a smooth single piece Plexiglas one. The rear of the canopy joins the high upper fuselage line continuously. The Bréguet 900 landed on a fixed monowheel undercarriage with a protective ash nose skid ahead of it. Unusually, the tow release involved two hooks, one on either side of the fuselage just under the wing leading edge.

The first prototype flew on 17 June 1948, the second in the following March.

Operational history

Soon after its first flight in March 1949 the second prototype, equipped with DFS airbrakes and flaps and flown by Paul Lepanse, set a new French distance record of 470 km (292 mi). This was later broken by Roger Biagi in the second production aircraft (900S-2) with a distance of 525 km (326 mi). 900S-4, piloted by Robert Delhoume, set a record speed around a 100 km (62 mi) triangle.

The 900 competed in two World Gliding Championships without success: in 1950 the second prototype was wrecked after an airbrake failure and in 1952 900S-5 was placed 21st out of 39, limited by its short span.

One restored Bréguet 900S, the first production machine, remains on the French civil register in 2010.

Variants

900

Two prototypes. 1st had spoilers and no flaps, 2nd DFS airbrakes and flaps.

900S

Six production aircraft, all slightly different: Schempp-Hirth airbrakes, a single piece canopy and a taller fin introduced piecemeal.

Specifications

Data from Sailplanes 1945-1965

General characteristics

• Capacity: 1
• Length: 6.50 m (21 ft 4 in)
• Wingspan: 14.35 m (47 ft 1 in)
• Wing area: 12.9 m² (139 sq ft)
• Aspect ratio: 15.85
• Airfoil: Breguet 14
• Empty weight: 211 kg (465 lb)
• Gross weight: 306 kg (675 lb)

Performance

• Maximum speed: 180 km/h (112 mph; 97 kn)
• Stall speed: 40 km/h (25 mph; 22 kn) with 30° flaps
• Maximum glide ratio: best 27:1 at 78 km/h; 42 kn (48 mph)
• Rate of sink: 0.75 m/s (148 ft/min) minimum at73 km/h; 39 kn (45 mph)
• Wing loading: 23.8 kg/m² (4.9 lb/sq ft)