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The LS10 differs from the LS6 mainly in its wing; its other features are similar. The aerofoil was derived from the FX 81-K-130 profile used in the LS6, having as improvements: higher performance at the low and high ends of the speed range, and very low sensitivity to turbulence, rain and bugs. The
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The ballast system has six integral tanks in the wings. The outboard tanks are filled first and dumped last for better spanwise load distribution. The tail ballast system incorporates two separate tanks to maintain a favourable C.G. during water dumping. The control of the first tail tank is
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In July 2007, Rick
Walters placed first in an LS10 at the International Lilienthal Glide 2007 which is the combined Pre-World for the 30th World Gliding Championships and the 2007 German nationals in the 15M and Open Class, in LĂŒsse Berlin.
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The wing was built in four parts with interchangeable wing tips, giving 15 or 18 metre span. The partition line for the wing extensions was located considerably inboard in the prototype, a feature that first appeared in the
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A taller undercarriage increases ground clearance and gives a higher angle of attack than an LS6, allowing a lower speed for take-off and landing. This increases safety when aerotowing from short runways and when landing
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for both spans and easier rigging. For series production DG-Flugzeugbau gave greater priority to structural and manufacturing considerations and the partition was moved outboard to seven metres from the fuselage axis.
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wings have turbulator tape on the underside to prevent laminar separation bubbles. This suggests the profile lacks the clean natural transition of the
Wortmann profile of 1981 and is probably more extensively laminar.
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There were two models in production: the âturboâ version called the LS10-st, with the same engine installation as the LS8-st; and the LS10-s with just an engine compartment for
200:. Certification was not achieved until 2010. Other gliders were designed and manufactured by competitors during this period and were produced in greater numbers.
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231:. Werner Scholz then developed the prototype, the LS10-a. Although early 3-view drawings of the LS10 showed a curved canopy rail similar to that of the
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It achieved certification in
January 2010, but it is no longer listed as a current product by DG Flugzeugbau.
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connected to the four outer wing tanks, the second tail tank operates with to the two inner wing tanks.
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By the mid-nineties
Rolladen-Schneider, prompted by customers, began designing a successor to the
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in Nitra, Slovakia. The flying qualities were reported in the German aviation magazine,
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The LS10 has the typical LS full-span flaperons and large, double-blade air brakes, and
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After
Rolladen-Schneider was placed in receivership the sailplane entered production by
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on 6 June 2003. This was followed by extensive flight-testing and then evaluation in
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The initial design had an elliptical leading edge similar to the
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Marzinzik G, LS10: Meistermacher?, Aerokurier, Aug 2004
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projects had higher priority and the company's owner,
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227:The initial design was made under the direction of
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429:280 km/h (175 mph, 152 kn)
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77:Learn how and when to remove this message
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40:This article includes a list of general
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224:, felt the LS6 was still competitive.
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212:. Development was protracted, as the
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381:18.00 m (59 ft 1 in)
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375:6.72 m (22 ft 1 in)
46:it lacks sufficient corresponding
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393:11.4 m (123 sq ft)
387:1.33 m (4 ft 4 in)
189:sailplane designed in Germany by
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441:0.50 m/s (100 ft/min)
348:Specifications (with 18m wings)
238:The first flight took place at
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369:190 kg (418 lb) water ballast
193:. A prototype flew in 2003.
632:Aircraft first flown in 2003
474:Aerokurier Aviation Magazine
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627:Rolladen-Schneider aircraft
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414:600 kg (1,320 lb)
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408:305 kg (671 lb)
317:and which allows optimal
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622:2000s German sailplanes
354:General characteristics
183:Rolladen-Schneider LS10
61:more precise citations.
18:Rolladen-Schneider LS10
484:DG Flugzeugbau website
469:DG-Flugzeugbau website
248:European Championships
204:Design and development
326:Other design features
433:Maximum glide ratio:
528:Single seat gliders
256:, to be excellent.
115:General information
520:Rolladen-Schneider
274:Design of the wing
191:Rolladen-Schneider
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233:Schleicher ASW 24
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98:The LS10-a and a
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16:(Redirected from
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589:Two seat gliders
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222:Walter Schneider
154:Production ended
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131:National origin
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172:First flight
159:Number built
140:Manufacturer
104:Niederöblarn
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420:Performance
175:6 June 2003
59:introducing
616:Categories
596:LSD Ornith
463:References
391:Wing area:
253:Aerokurier
229:Wolf Lemke
42:references
379:Wingspan:
367:Capacity:
363:One pilot
315:Ventus 2c
240:Egelsbach
126:sailplane
446:See also
319:planform
302:and the
300:Discus-2
284:SZD-55-1
187:18 metre
385:Height:
373:Length:
296:DG-1000
288:LAK-17a
167:History
134:Germany
108:Austria
100:DG-808B
55:improve
435:>50
292:ASW 28
185:is an
151:Status
44:, but
361:Crew:
341:HĂ€nle
601:LS11
580:LS10
402:28.4
336:out.
216:and
181:The
120:Type
92:LS10
575:LS9
570:LS8
565:LS7
560:LS6
555:LS5
550:LS4
545:LS3
540:LS2
535:LS1
306:).
304:eta
218:LS9
214:LS8
210:LS6
102:at
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