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two-blade propeller were finally selected. The engine installation, including the carbon composite propeller mast and folding exhaust system, was developed by the specialist firm
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The LS9 was the sole self-launching glider developed at
Rolladen-Schneider. The prototype first flew in 1995, powered by a
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All-new structure combining a new safety glass/carbon cockpit with a full carbon composite fuselage behind the wing.
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Innovative 210 mm x 65 mm steerable tailwheel integrated into the rudder directly under the hinge axis.
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Larger undercarriage (5” hub) set further forward to prevent nose-over with the engine at full power.
172:. Production ended after just 10 gliders were built, when Rolladen-Schneider went into receivership.
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Engine recessed into the fuselage with electric starter, fuel and coolant pumps.
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Carbon composite propeller mast deployed by electric screw jack system.
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Thomas F, Fundamentals of
Sailplane Design, College Park Press, 1999
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Ewald J, Flight Test of the LS-9, Sailplane and
Gliding, Oct. 2000
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two-stroke engine. Production of this engine was discontinued by
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Newsletter of the
Auxiliary Powered Sailplane Association
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by broadening the tail boom to accommodate the engine.
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Stall warning system activated during powered flight.
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220:moulds, with strengthened spars and leading edges.
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255:Drive belt transmission to the large propeller.
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233:Empennage from the LS4 with new carbon and
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203:, having nearly 100% commonality with the
348:270 km/h (170 mph, 150 kn)
69:Learn how and when to remove this message
32:This article includes a list of general
354:550 km (340 mi, 300 nmi)
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16:Single seat German motor glider, 1994
18:
410:Website of LS dealer Solaire Canada
290:18.00 m (59 ft 1 in)
13:
284:6.84 m (22 ft 5 in)
38:it lacks sufficient corresponding
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302:11.4 m (123 sq ft)
296:1.43 m (4 ft 8 in)
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223:Fuselage shape adapted from the
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372:0.58 m/s (114 ft/min)
366:4.0 m/s (780 ft/min)
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1:
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246:Single aerotow/winching hook.
201:Walter Binder Motorenbau GmbH
564:Aircraft first flown in 1995
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559:Rolladen-Schneider aircraft
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323:525 kg (1,155 lb)
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333:, 41 kW (55 hp)
317:350 kg (770 lb)
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554:2000s German sailplanes
269:General characteristics
237:composite construction.
205:Schempp-Hirth Ventus CM
53:more precise citations.
400:LS-Flugzeugbau website
158:Rolladen-Schneider LS9
358:Maximum glide ratio:
168:launched in 2000 by
460:Single seat gliders
98:General information
452:Rolladen-Schneider
170:Rolladen-Schneider
128:Rolladen-Schneider
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569:T-tail aircraft
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388:List of gliders
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216:Wings from the
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114:National origin
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45:Please help to
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59:December 2012
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454:glider types
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307:Aspect ratio
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166:motor glider
164:single-seat
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147:First flight
134:Number built
123:Manufacturer
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339:Performance
327:Powerplant:
176:Development
109:motorglider
51:introducing
548:Categories
528:LSD Ornith
394:References
300:Wing area:
197:Technoflug
34:references
331:Solo 2625
288:Wingspan:
193:Solo 2625
182:Rotax 535
377:See also
162:18 metre
294:Height:
282:Length:
218:LS6-18w
142:History
117:Germany
47:improve
360:>47
352:Range:
235:aramid
211:Design
160:is an
36:, but
276:Crew:
186:Rotax
533:LS11
512:LS10
329:1 ×
311:28.4
191:The
156:The
150:1995
103:Type
507:LS9
502:LS8
497:LS7
492:LS6
487:LS5
482:LS4
477:LS3
472:LS2
467:LS1
278:One
225:LS4
84:LS9
550::
137:10
444:e
437:t
430:v
309::
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66:(
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