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Antonov A-15 Contents Design and development Operational history Specifications (Antonov A-15) See also Notes References External links Navigation menu"A-15 Antonov""The Incomplete Guide to Airfoil Usage"Archived"Make / Model Inquiry Results""A-15 Antonov""The Incomplete Guide to Airfoil Usage"Archived"Make / Model Inquiry Results"A-15 Three viewPhoto of the A-15Video of A-15 landinge

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Soviet sailplanes 1960–1969Antonov aircraftGlider aircraftAircraft first flown in 1960


Sovietmid-wingV-tailedFAI Open ClassgliderOleg AntonovAntonovA-11A-13aluminiumCold WarAmericanNACAairfoilwing rootwingtipFederal Aviation AdministrationUnited States












Antonov A-15




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A-15

Antonow A-15 1999 by Jiri Havlice.jpg
Antonov A-15 registered in the Czech Republic
Role

Glider

National origin

USSR
Manufacturer

Antonov
Designer

Oleg Antonov
First flight
26 March 1960

Number built
350

The Antonov A-15 is a Soviet mid-wing, V-tailed single-seat, FAI Open Class glider that was designed by Oleg Antonov and produced by Antonov.[1]




Contents





  • 1 Design and development


  • 2 Operational history


  • 3 Specifications (Antonov A-15)


  • 4 See also


  • 5 Notes


  • 6 References


  • 7 External links




Design and development


The A-15 was a follow-on design, based on the bureau's experience gained with the A-11 and A-13 gliders. This new open class design quickly proved its worth as a record-setter.[1]


The aircraft is made from aluminium. Unusually for a Cold War Soviet aircraft, its 17 m (55.8 ft) span wing employs an American NACA 64-618 airfoil at the wing root, transitioning to an NACA 64-616 section at the wingtip. The A-15 carries 50 kg (110 lb) of water ballast. The landing gear is a retractable monowheel.[1][2]


A total of 350 A-15s were built.[1]



Operational history


The A-15 was used to set many world records, including a world goal distance record of 714.023 km (444 mi), flown in June 1960.[1]


In August 2011, there was one A-15 registered with the Federal Aviation Administration in the United States.[3]



Specifications (Antonov A-15)


Data from The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II[4] Sailplane Directory[1]


General characteristics



  • Crew: one


  • Length: 7.2 m (23 ft 7 in)


  • Wingspan: 17 m (55 ft 9 in)


  • Height: 1.15 m (3 ft 9 in) at cockpit


  • Wing area: 12 m2 (130 sq ft)


  • Aspect ratio: 24


  • Airfoil: Root: NACA 643618, Tip: NACA 633616


  • Empty weight: 273 kg (602 lb)


  • Gross weight: 380 kg (838 lb)

Performance



  • Stall speed: 55 km/h (34 mph; 30 kn)


  • Never exceed speed: 250 km/h (155 mph; 135 kn)


  • Rough air speed max: 250 km/h (155.3 mph; 135.0 kn)


  • Aerotow speed: 140 km/h (87.0 mph; 75.6 kn)


  • Winch launch speed: 120 km/h (74.6 mph; 64.8 kn)


  • g limits: +7.5 -3 at 250 km/h (155.3 mph; 135.0 kn)


  • Maximum glide ratio: 40 at 100 km/h (62.1 mph; 54.0 kn)


  • Rate of sink: 0.6 m/s (120 ft/min) at 90 km/h (55.9 mph; 48.6 kn)


  • Wing loading: 31.6 kg/m2 (6.5 lb/sq ft)


See also



Related development


  • Antonov A-9

  • Antonov A-11

  • Antonov A-13



Related lists


  • List of gliders


Notes




  1. ^ abcdef Activate Media (2006). "A-15 Antonov". Retrieved 8 August 2011..mw-parser-output cite.citationfont-style:inherit.mw-parser-output .citation qquotes:"""""""'""'".mw-parser-output .citation .cs1-lock-free abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/6/65/Lock-green.svg/9px-Lock-green.svg.png")no-repeat;background-position:right .1em center.mw-parser-output .citation .cs1-lock-limited a,.mw-parser-output .citation .cs1-lock-registration abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/d/d6/Lock-gray-alt-2.svg/9px-Lock-gray-alt-2.svg.png")no-repeat;background-position:right .1em center.mw-parser-output .citation .cs1-lock-subscription abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/a/aa/Lock-red-alt-2.svg/9px-Lock-red-alt-2.svg.png")no-repeat;background-position:right .1em center.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registrationcolor:#555.mw-parser-output .cs1-subscription span,.mw-parser-output .cs1-registration spanborder-bottom:1px dotted;cursor:help.mw-parser-output .cs1-ws-icon abackground:url("//upload.wikimedia.org/wikipedia/commons/thumb/4/4c/Wikisource-logo.svg/12px-Wikisource-logo.svg.png")no-repeat;background-position:right .1em center.mw-parser-output code.cs1-codecolor:inherit;background:inherit;border:inherit;padding:inherit.mw-parser-output .cs1-hidden-errordisplay:none;font-size:100%.mw-parser-output .cs1-visible-errorfont-size:100%.mw-parser-output .cs1-maintdisplay:none;color:#33aa33;margin-left:0.3em.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration,.mw-parser-output .cs1-formatfont-size:95%.mw-parser-output .cs1-kern-left,.mw-parser-output .cs1-kern-wl-leftpadding-left:0.2em.mw-parser-output .cs1-kern-right,.mw-parser-output .cs1-kern-wl-rightpadding-right:0.2em


  2. ^ Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". Archived from the original on 19 July 2011. Retrieved 8 August 2011.


  3. ^ Federal Aviation Administration (August 2011). "Make / Model Inquiry Results". Retrieved 15 August 2011.


  4. ^ Shenstone, B.S.; K.G. Wilkinson (1963). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II (in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 245–246.




References


.mw-parser-output .refbeginfont-size:90%;margin-bottom:0.5em.mw-parser-output .refbegin-hanging-indents>ullist-style-type:none;margin-left:0.mw-parser-output .refbegin-hanging-indents>ul>li,.mw-parser-output .refbegin-hanging-indents>dl>ddmargin-left:0;padding-left:3.2em;text-indent:-3.2em;list-style:none.mw-parser-output .refbegin-100font-size:100%


  • Shenstone, B.S.; K.G. Wilkinson (1963). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II (in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 245–246.


  • Activate Media (2006). "A-15 Antonov". Retrieved 8 August 2011.


  • Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". Archived from the original on 19 July 2011. Retrieved 8 August 2011.


  • Federal Aviation Administration (August 2011). "Make / Model Inquiry Results". Retrieved 15 August 2011.



External links




  • A-15 Three view

  • Photo of the A-15

  • Video of A-15 landing









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