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Cadet UT-1

The Cadet UT-1 is an American single-seat, high wing, strut-braced glider modified by Alex Dawydoff from the original Slingsby Kirby Cadet design and produced by Cadet Aeronautics.[1]

UT-1
Role Glider
National origin United States
Manufacturer Cadet Aeronautics
Designer Alex Dawydoff
First flight 1943
Introduction 1943
Status Prototype only produced
Produced 1943
Number built One
Developed from Slingsby Kirby Cadet

Design and development edit

In 1942 Dawydoff obtained the plans and the rights to produce the Slingsby Cadet under licence from Fred Slingsby. Dawydoff had the plans redrawn to US measurements, the structural strength increased, plus a new tow hook and wing rigging design. The wing is assembled using just one 4 ft (1.2 m) long pin per wing.[1]

The UT-1 is built predominantly from wood, with the fuselage wooden framed and covered in plywood. The wing and tail are also wooden-framed and covered in doped aircraft fabric covering. The two-spar wing is supported by dual struts.[1]

Dawydoff's plan was to gain government support to provide the UT-1 in kit form for assembly by schools and clubs. The government money was not forthcoming and the post-war period saw a large number of surplus military training gliders saturate the market. As a result, only one UT-1 was completed. It is now located in the National Soaring Museum.[1][2]

Aircraft on display edit

Specifications (UT-1) edit

Data from Soaring[1]

General characteristics

  • Crew: one
  • Wingspan: 38 ft 5 in (11.71 m)
  • Wing area: 172.5 sq ft (16.03 m2)
  • Aspect ratio: 8.5:1
  • Airfoil: Go 426
  • Empty weight: 276 lb (125 kg)
  • Gross weight: 450 lb (204 kg)

Performance

  • Maximum glide ratio: 14.7:1 at 30 mph (48 km/h)
  • Rate of sink: 210 ft/min (1.1 m/s) at 28 mph (45 km/h)
  • Wing loading: 2.6 lb/sq ft (13 kg/m2)

See also edit

References edit

  1. ^ a b c d e Said, Bob: 1983 Sailplane Directory, Soaring Magazine, page 39. Soaring Society of America November 1983. USPS 499-920
  2. ^ a b National Soaring Museum (2011). . Archived from the original on May 16, 2011. Retrieved May 5, 2011.

cadet, american, single, seat, high, wing, strut, braced, glider, modified, alex, dawydoff, from, original, slingsby, kirby, cadet, design, produced, cadet, aeronautics, role, glider, national, origin, united, states, manufacturer, cadet, aeronautics, designer. The Cadet UT 1 is an American single seat high wing strut braced glider modified by Alex Dawydoff from the original Slingsby Kirby Cadet design and produced by Cadet Aeronautics 1 UT 1 Role Glider National origin United States Manufacturer Cadet Aeronautics Designer Alex Dawydoff First flight 1943 Introduction 1943 Status Prototype only produced Produced 1943 Number built One Developed from Slingsby Kirby Cadet Contents 1 Design and development 2 Aircraft on display 3 Specifications UT 1 4 See also 5 ReferencesDesign and development editIn 1942 Dawydoff obtained the plans and the rights to produce the Slingsby Cadet under licence from Fred Slingsby Dawydoff had the plans redrawn to US measurements the structural strength increased plus a new tow hook and wing rigging design The wing is assembled using just one 4 ft 1 2 m long pin per wing 1 The UT 1 is built predominantly from wood with the fuselage wooden framed and covered in plywood The wing and tail are also wooden framed and covered in doped aircraft fabric covering The two spar wing is supported by dual struts 1 Dawydoff s plan was to gain government support to provide the UT 1 in kit form for assembly by schools and clubs The government money was not forthcoming and the post war period saw a large number of surplus military training gliders saturate the market As a result only one UT 1 was completed It is now located in the National Soaring Museum 1 2 Aircraft on display editNational Soaring Museum 1 2 Specifications UT 1 editData from Soaring 1 General characteristicsCrew one Wingspan 38 ft 5 in 11 71 m Wing area 172 5 sq ft 16 03 m2 Aspect ratio 8 5 1 Airfoil Go 426 Empty weight 276 lb 125 kg Gross weight 450 lb 204 kg Performance Maximum glide ratio 14 7 1 at 30 mph 48 km h Rate of sink 210 ft min 1 1 m s at 28 mph 45 km h Wing loading 2 6 lb sq ft 13 kg m2 See also editList of glidersReferences edit a b c d e Said Bob 1983 Sailplane Directory Soaring Magazine page 39 Soaring Society of America November 1983 USPS 499 920 a b National Soaring Museum 2011 Sailplanes in Our Collection Archived from the original on May 16 2011 Retrieved May 5 2011 Retrieved from https en wikipedia org w index php title Cadet UT 1 amp oldid 1066043869, wikipedia, wiki, book, books, library,

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