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Schleicher ASW 27

The ASW 27 is a 15 metre Class glider built of modern fibre reinforced composites, which first flew in 1995 and was certified in 1997. The manufacturer of the ASW 27 is Alexander Schleicher GmbH & Co. The "W" indicates this is a design of the influential and prolific German designer Gerhard Waibel.

ASW 27
Role 15 metre-class sailplane
National origin Germany
Manufacturer Schleicher
Designer Gerhard Waibel
First flight 1995
Number built 237 by 2009
External image
Schleicher ASW 27 on aerotow

Design and development edit

The ASW 27 has plain flaps, winglets, a retractable undercarriage and a water ballast system. The ASW 27 superseded the ASW 20 in the manufacturer's production line.

The structure is a complex composite of carbon, aramid and polyethylene fibre reinforced plastic. This permits a light structure with the strength to carry large amounts of water ballast, thus permitting the widest possible range of wing loadings for weak and strong soaring weather. The strong fuselage was tested for crash protection by dropping one from a crane.

The winglets were standard equipment from the beginning, but were later enlarged in the ASW-27B development. The "B" also has tanks to hold water ballast rather than bags. The ASW 27 does not have a version with wing extensions for 18 metres. This was a design decision to pursue an uncompromised 15 metre racer, as "future engine retrofits or later wingspan increases were specifically ruled out".

The introduction of the ASG 29 gave the ASW 27 a stablemate that can compete in the same class, although the 29 is intended to fly primarily with an 18-metre span and can be motorised. Because of the overlap with the ASG 29, production of the ASW27 has now ceased.

Specifications edit

Data from flight manual [1]

General characteristics

  • Crew: 1
  • Length: 6.55 m (21 ft 6 in)
  • Wingspan: 15 m (49 ft 3 in)
  • Wing area: 9 m2 (97 sq ft)
  • Aspect ratio: 25
  • Airfoil: Root: DU 89-134/14, Tip: DU 94-086 M4
  • Empty weight: 245 kg (540 lb)
  • Gross weight: 500 kg (1,102 lb)

Performance

  • Never exceed speed: 285 km/h (177 mph, 154 kn)
  • Rough air speed max: 215 km/h (134 mph; 116 kn)
  • Aerotow speed: 170 km/h (110 mph; 92 kn)
  • Winch launch speed: 130 km/h (81 mph; 70 kn)
  • Minimum control speed: 70 km/h (43 mph, 38 kn) with no ballast and full flaps
  • g limits: +5.3 -2.65 at 215 km/h (134 mph; 116 kn)
  • Maximum glide ratio: 48
  • Rate of sink: 0.58 m/s (114 ft/min) (minimum)

See also edit

Related lists

References edit

  1. ^ Flight manual, Schleicher
  • Alexander Schleicher GmbH & Co
  • Sailplane Directory
  • Simons M, Segelflugzeuge 1965–2000, Equip, 2004

schleicher, this, article, includes, list, general, references, lacks, sufficient, corresponding, inline, citations, please, help, improve, this, article, introducing, more, precise, citations, december, 2012, learn, when, remove, this, message, metre, class, . This article includes a list of general references but it lacks sufficient corresponding inline citations Please help to improve this article by introducing more precise citations December 2012 Learn how and when to remove this message The ASW 27 is a 15 metre Class glider built of modern fibre reinforced composites which first flew in 1995 and was certified in 1997 The manufacturer of the ASW 27 is Alexander Schleicher GmbH amp Co The W indicates this is a design of the influential and prolific German designer Gerhard Waibel ASW 27 Role 15 metre class sailplane National origin Germany Manufacturer Schleicher Designer Gerhard Waibel First flight 1995 Number built 237 by 2009 External imageSchleicher ASW 27 on aerotow Contents 1 Design and development 2 Specifications 3 See also 4 ReferencesDesign and development editThe ASW 27 has plain flaps winglets a retractable undercarriage and a water ballast system The ASW 27 superseded the ASW 20 in the manufacturer s production line The structure is a complex composite of carbon aramid and polyethylene fibre reinforced plastic This permits a light structure with the strength to carry large amounts of water ballast thus permitting the widest possible range of wing loadings for weak and strong soaring weather The strong fuselage was tested for crash protection by dropping one from a crane The winglets were standard equipment from the beginning but were later enlarged in the ASW 27B development The B also has tanks to hold water ballast rather than bags The ASW 27 does not have a version with wing extensions for 18 metres This was a design decision to pursue an uncompromised 15 metre racer as future engine retrofits or later wingspan increases were specifically ruled out The introduction of the ASG 29 gave the ASW 27 a stablemate that can compete in the same class although the 29 is intended to fly primarily with an 18 metre span and can be motorised Because of the overlap with the ASG 29 production of the ASW27 has now ceased Specifications editData from flight manual 1 General characteristicsCrew 1 Length 6 55 m 21 ft 6 in Wingspan 15 m 49 ft 3 in Wing area 9 m2 97 sq ft Aspect ratio 25 Airfoil Root DU 89 134 14 Tip DU 94 086 M4 Empty weight 245 kg 540 lb Gross weight 500 kg 1 102 lb Performance Never exceed speed 285 km h 177 mph 154 kn Rough air speed max 215 km h 134 mph 116 kn Aerotow speed 170 km h 110 mph 92 kn Winch launch speed 130 km h 81 mph 70 kn Minimum control speed 70 km h 43 mph 38 kn with no ballast and full flaps g limits 5 3 2 65 at 215 km h 134 mph 116 kn Maximum glide ratio 48 Rate of sink 0 58 m s 114 ft min minimum See also editRelated lists List of glidersReferences edit nbsp Wikimedia Commons has media related to Schleicher ASW 27 Flight manual Schleicher Alexander Schleicher GmbH amp Co Sailplane Directory Simons M Segelflugzeuge 1965 2000 Equip 2004 Retrieved from https en wikipedia org w index php title Schleicher ASW 27 amp oldid 1191090090, wikipedia, wiki, book, books, library,

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