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Oškinis BRO-16

The Oškinis BRO-16, sometimes known as the Oškinis BRO-16 Pempė (Pempė in Lithuanian translates as Northern Lapwing), was a flying boat, biplane training glider, flown and produced in the USSR in the 1970s.

BRO-16
Role Flying boat, biplane training glider
National origin USSR
Designer Bronis Oškinis
First flight August 1973

Design and development edit

The BRO-16 was a single-seat training glider, unusual for being both a biplane and a flying boat. It was a development of the BRO-11 land monoplane produced some twenty years earlier and first flew in August 1973.[1]

Its wings were rectangular in plan out to rounded tips. The lower wing was 25% shorter in span than the upper but with about the same chord and ply-covered in contrast to the fabric covered upper wing. Both wings had single-spar structures and were braced together with wide spread, transverse, streamlined and distorted V-struts between the spars. There was no stagger, 3° of dihedral and a large interplane gap. The BRO-16's push-rod activated, fabric-covered ailerons, which could also serve as flaps, were suspended from the upper wing and filled 87% of the span.[1]

The BRO-19's fuselage had a forward nacelle attached to a flat girder fuselage supporting the tail. The largely wooden nacelle was 3.70 m (12 ft 2 in) long and flat-bottomed. The cockpit, close to the nose, was open and placed the pilot over the leading edge of the lower wing which was mounted on the side of the nacelle, about halfway back. The rear of the fuselage was formed by a horizontal girder member, just under the upper wing, attached to the nacelle with a pair of vertical struts between the wings and an oblique strut from the rear of the nacelle to the top of the aft vertical strut. Wires braced the rear fuselage to the wing struts and to the nacelle. Parts of the girder were canvas-covered.[1]

The tail was conventional. Though the triangular fin was very small, the rudder was large, nearly rectangular in profile apart from a blunted top and a slightly angled underside. The tailplane was triangular in plan and carried rectangular elevators. All the tail surfaces were fabric-covered wooden structures.[1]

Operational history edit

The BRO-16 was mass produced, though numbers are not available. They operated from the Lithuanian Kaunas Reservoir.[2]

Variants edit

BRO-16 Pempė
main production variant.
BRO-17U Utochka
Short span (7.00 m (23 ft 0 in) variant. Rectangular plan wings, the upper divided into three staggered, overhanging slats. Completion uncertain.[1]

Specifications (BRO-16) edit

Data from Jane's All the World's Aircraft 1975-76[3]

General characteristics

  • Crew: one
  • Length: 5.24 m (17 ft 2 in)
  • Upper wingspan: 7 m (23 ft 0 in)
  • Lower wingspan: 5.8 m (19 ft 0 in)
  • Height: 3.65 m (12 ft 0 in)
  • Wing area: 8.26 m2 (88.9 sq ft) upper
6.00 m2 (64.58 sq ft) lower
  • Aspect ratio: 3.8:1
  • Airfoil: TsAGI R-II (14%)
  • Aileron section: TsAGI R-III (16%)
  • Empty weight: 129 kg (284 lb)
  • Max takeoff weight: 204 kg (450 lb)
  • Dihedral: 3° 24' on both upper and lower wings
  • Incidence:

Performance

  • Wing loading: 12.3 kg/m2 (2.5 lb/sq ft)

References edit

  1. ^ a b c d e Taylor, John W R (1977). Jane's All the World's Aircraft 1977-78. London: Jane's Yearbooks. p. 619-20. ISBN 0-354-00551-0.
  2. ^ "BRO-16". Retrieved 14 August 2019.
  3. ^ Taylor, John W.R., ed. (1975). Jane's all the world's aircraft 1975–76 (66th annual ed.). New York: Franklin Watts Inc. pp. 603–604. ISBN 978-0531032503.

oškinis, sometimes, known, pempė, pempė, lithuanian, translates, northern, lapwing, flying, boat, biplane, training, glider, flown, produced, ussr, 1970s, role, flying, boat, biplane, training, glider, national, origin, ussr, designer, bronis, oškinis, first, . The Oskinis BRO 16 sometimes known as the Oskinis BRO 16 Pempe Pempe in Lithuanian translates as Northern Lapwing was a flying boat biplane training glider flown and produced in the USSR in the 1970s BRO 16 Role Flying boat biplane training glider National origin USSR Designer Bronis Oskinis First flight August 1973 Contents 1 Design and development 2 Operational history 3 Variants 4 Specifications BRO 16 5 ReferencesDesign and development editThe BRO 16 was a single seat training glider unusual for being both a biplane and a flying boat It was a development of the BRO 11 land monoplane produced some twenty years earlier and first flew in August 1973 1 Its wings were rectangular in plan out to rounded tips The lower wing was 25 shorter in span than the upper but with about the same chord and ply covered in contrast to the fabric covered upper wing Both wings had single spar structures and were braced together with wide spread transverse streamlined and distorted V struts between the spars There was no stagger 3 of dihedral and a large interplane gap The BRO 16 s push rod activated fabric covered ailerons which could also serve as flaps were suspended from the upper wing and filled 87 of the span 1 The BRO 19 s fuselage had a forward nacelle attached to a flat girder fuselage supporting the tail The largely wooden nacelle was 3 70 m 12 ft 2 in long and flat bottomed The cockpit close to the nose was open and placed the pilot over the leading edge of the lower wing which was mounted on the side of the nacelle about halfway back The rear of the fuselage was formed by a horizontal girder member just under the upper wing attached to the nacelle with a pair of vertical struts between the wings and an oblique strut from the rear of the nacelle to the top of the aft vertical strut Wires braced the rear fuselage to the wing struts and to the nacelle Parts of the girder were canvas covered 1 The tail was conventional Though the triangular fin was very small the rudder was large nearly rectangular in profile apart from a blunted top and a slightly angled underside The tailplane was triangular in plan and carried rectangular elevators All the tail surfaces were fabric covered wooden structures 1 Operational history editThe BRO 16 was mass produced though numbers are not available They operated from the Lithuanian Kaunas Reservoir 2 Variants editBRO 16 Pempe main production variant BRO 17U Utochka Short span 7 00 m 23 ft 0 in variant Rectangular plan wings the upper divided into three staggered overhanging slats Completion uncertain 1 Specifications BRO 16 editData from Jane s All the World s Aircraft 1975 76 3 General characteristicsCrew one Length 5 24 m 17 ft 2 in Upper wingspan 7 m 23 ft 0 in Lower wingspan 5 8 m 19 ft 0 in Height 3 65 m 12 ft 0 in Wing area 8 26 m2 88 9 sq ft upper 6 00 m2 64 58 sq ft lower dd dd dd Aspect ratio 3 8 1 Airfoil TsAGI R II 14 Aileron section TsAGI R III 16 Empty weight 129 kg 284 lb Max takeoff weight 204 kg 450 lb Dihedral 3 24 on both upper and lower wings Incidence 3 Performance Wing loading 12 3 kg m2 2 5 lb sq ft References edit a b c d e Taylor John W R 1977 Jane s All the World s Aircraft 1977 78 London Jane s Yearbooks p 619 20 ISBN 0 354 00551 0 BRO 16 Retrieved 14 August 2019 Taylor John W R ed 1975 Jane s all the world s aircraft 1975 76 66th annual ed New York Franklin Watts Inc pp 603 604 ISBN 978 0531032503 Retrieved from https en wikipedia org w index php title Oskinis BRO 16 amp oldid 1101449209, wikipedia, wiki, book, books, library,

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