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Bréguet 902 Cinzano

The Bréguet Br 902 Cinzano was a French training glider produced in the 1950s by Société anonyme des Ateliers d'aviation Louis Bréguet

Br 902 Cinzano
Role Glider
National origin France
Manufacturer Société anonyme des Ateliers d'aviation Louis Bréguet
Designer Jean Cayla / R. Jarlaud
First flight 14 May 1957
Number built 6

Design and development edit

In response to a need for replacing the Caudron C.800 training glider with a contemporary high performance trainer, Bréguet designed and built the Br 902 Cinzano prototype, with parts in common with the Br 901 and Br 904. Production aircraft would have been optimised for production and also used new manufacturing techniques, particularly for the wings, which were intended to be built using the hollow shell method; high-accuracy plywood skins laid up in jig moulds with structure added in the mould to retain the high accuracy surfaces.[1]

Construction was of welded steel tube for the fuselage with wood for wings and empennage. The fuselage was covered in fabric, with plywood for areas requiring more resilience. Flying controls, wings and empennage were built up from wood with plywood high strength members, covered with fabric. The instructor and pupil sat in closed tandem cockpits covered with Plexiglass canopies. Control was via conventional ailerons, elevators, operated by rods and rudder operated by cables, with airbrakes on the wings for approach control. The undercarriage consisted of a single mainwheel fitted with a hydraulic brake, rubber sprung tail-skid, with protection skids on the wing-tips.[1]

The first prototype, Br 902-01, flew for the first time on 14 May 1957 piloted by Paul Lepanse, but despite good performance and flying characteristics, the Br 902 failed to sell well; only a small production run of 6 gliders was built.[1][2]

Specifications (Br 902) edit

Data from Planeurs: Breguet Br-902 Cinzano,[3] Aviafrance : Breguet Br 902,[2] OSTIV 1958[4]

General characteristics

  • Crew: 2
  • Length: 9 m (29 ft 6 in)
  • Wingspan: 18 m (59 ft 1 in)
  • Wing area: 21.6 m2 (233 sq ft)
  • Aspect ratio: 15
  • Airfoil: NACA 63 modified
  • Empty weight: 330 kg (728 lb)
  • Gross weight: 500 kg (1,102 lb)

Performance

  • Stall speed: 60 km/h (37 mph, 32 kn)
  • Never exceed speed: 220 km/h (140 mph, 120 kn)
  • Maximum glide ratio: 28 at 78 km/h (48 mph; 42 kn)
  • Rate of sink: 0.7 m/s (140 ft/min) at 65 km/h (40 mph; 35 kn)
  • Wing loading: 23 kg/m2 (4.7 lb/sq ft)

References edit

  1. ^ a b c Cuny, Jean; Leyvastre, Pirre. Les Avions Breguet (1940/1971). Paris: Docavia. pp. 116–117.
  2. ^ a b Parmentier, Bruno (18 June 2000). "Breguet Br 902". Aviafrance (in French). Paris. Retrieved 28 January 2019.
  3. ^ "Breguet Br-902 Cinzano". www.j2mcl-planeurs.net (in French). 22 September 2016. Retrieved 28 January 2019.
  4. ^ Shenstone, B.S.; K.G. Wilkinson (1958). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde (in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 38–40.

Bibliography edit

  • Cuny, Jean & Leyvastre, Pierre (1977). Les Avions Breguet (1940/1971). DOCAVIA (in French). Vol. 6. Paris: Editions Larivière. OCLC 440863702.
  • Lacaze, Henri (2016). Les avions Louis Breguet Paris [The Aircraft of Louis Breguet, Paris] (in French). Vol. 2: le règne du monoplan. Le Vigen, France. ISBN 978-2-914017-89-3.{{cite book}}: CS1 maint: location missing publisher (link)

bréguet, cinzano, bréguet, cinzano, french, training, glider, produced, 1950s, société, anonyme, ateliers, aviation, louis, bréguetbr, cinzanorole, glidernational, origin, francemanufacturer, société, anonyme, ateliers, aviation, louis, bréguetdesigner, jean, . The Breguet Br 902 Cinzano was a French training glider produced in the 1950s by Societe anonyme des Ateliers d aviation Louis BreguetBr 902 CinzanoRole GliderNational origin FranceManufacturer Societe anonyme des Ateliers d aviation Louis BreguetDesigner Jean Cayla R JarlaudFirst flight 14 May 1957Number built 6 Contents 1 Design and development 2 Specifications Br 902 3 References 4 BibliographyDesign and development editIn response to a need for replacing the Caudron C 800 training glider with a contemporary high performance trainer Breguet designed and built the Br 902 Cinzano prototype with parts in common with the Br 901 and Br 904 Production aircraft would have been optimised for production and also used new manufacturing techniques particularly for the wings which were intended to be built using the hollow shell method high accuracy plywood skins laid up in jig moulds with structure added in the mould to retain the high accuracy surfaces 1 Construction was of welded steel tube for the fuselage with wood for wings and empennage The fuselage was covered in fabric with plywood for areas requiring more resilience Flying controls wings and empennage were built up from wood with plywood high strength members covered with fabric The instructor and pupil sat in closed tandem cockpits covered with Plexiglass canopies Control was via conventional ailerons elevators operated by rods and rudder operated by cables with airbrakes on the wings for approach control The undercarriage consisted of a single mainwheel fitted with a hydraulic brake rubber sprung tail skid with protection skids on the wing tips 1 The first prototype Br 902 01 flew for the first time on 14 May 1957 piloted by Paul Lepanse but despite good performance and flying characteristics the Br 902 failed to sell well only a small production run of 6 gliders was built 1 2 Specifications Br 902 editData from Planeurs Breguet Br 902 Cinzano 3 Aviafrance Breguet Br 902 2 OSTIV 1958 4 General characteristicsCrew 2 Length 9 m 29 ft 6 in Wingspan 18 m 59 ft 1 in Wing area 21 6 m2 233 sq ft Aspect ratio 15 Airfoil NACA 63 modified Empty weight 330 kg 728 lb Gross weight 500 kg 1 102 lb Performance Stall speed 60 km h 37 mph 32 kn Never exceed speed 220 km h 140 mph 120 kn Maximum glide ratio 28 at 78 km h 48 mph 42 kn Rate of sink 0 7 m s 140 ft min at 65 km h 40 mph 35 kn Wing loading 23 kg m2 4 7 lb sq ft References edit a b c Cuny Jean Leyvastre Pirre Les Avions Breguet 1940 1971 Paris Docavia pp 116 117 a b Parmentier Bruno 18 June 2000 Breguet Br 902 Aviafrance in French Paris Retrieved 28 January 2019 Breguet Br 902 Cinzano www j2mcl planeurs net in French 22 September 2016 Retrieved 28 January 2019 Shenstone B S K G Wilkinson 1958 The World s Sailplanes Die Segelflugzeuge der Welt Les Planeurs du Monde in English French and German 1st ed Zurich Organisation Scientifique et Technique Internationale du Vol a Voile OSTIV and Schweizer Aero Revue pp 38 40 Bibliography editCuny Jean amp Leyvastre Pierre 1977 Les Avions Breguet 1940 1971 DOCAVIA in French Vol 6 Paris Editions Lariviere OCLC 440863702 Lacaze Henri 2016 Les avions Louis Breguet Paris The Aircraft of Louis Breguet Paris in French Vol 2 le regne du monoplan Le Vigen France ISBN 978 2 914017 89 3 a href Template Cite book html title Template Cite book cite book a CS1 maint location missing publisher link Retrieved from https en wikipedia org w index php title Breguet 902 Cinzano amp oldid 1215200554, wikipedia, wiki, book, books, library,

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