The Rolladen-Schneider LS9 is an 18 metre single-seat motor glider launched in 2000 by Rolladen-Schneider. Production ended after just 10 gliders were built, when Rolladen-Schneider went into receivership.
The LS9 was the sole self-launching glider developed at Rolladen-Schneider. The prototype first flew in 1995, powered by a Rotax 535 two-stroke engine. Production of this engine was discontinued by Rotax, putting the LS9 project on hold pending the development of a suitable engine.
The Solo 2625 engine and a Technoflug 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 Walter Binder Motorenbau GmbH, having nearly 100% commonality with the Schempp-Hirth Ventus CM installation.
Designedit
Wings from the LS6-18w moulds, with strengthened spars and leading edges.
Fuselage shape adapted from the LS4 by broadening the tail boom to accommodate the engine.
All-new structure combining a new safety glass/carbon cockpit with a full carbon composite fuselage behind the wing.
Empennage from the LS4 with new carbon and aramid composite construction.
Larger undercarriage (5” hub) set further forward to prevent nose-over with the engine at full power.
Innovative 210 mm x 65 mm steerable tailwheel integrated into the rudder directly under the hinge axis.
Single aerotow/winching hook.
Carbon composite propeller mast deployed by electric screw jack system.
Engine recessed into the fuselage with electric starter, fuel and coolant pumps.
Drive belt transmission to the large propeller.
Stall warning system activated during powered flight.
Wikimedia Commons has media related to Rolladen-Schneider LS9.
Website of LS dealer Solaire Canada
Thomas F, Fundamentals of Sailplane Design, College Park Press, 1999
Ewald J, Flight Test of the LS-9, Sailplane and Gliding, Oct. 2000
January 01, 1970
rolladen, schneider, 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. 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 Rolladen Schneider LS9 is an 18 metre single seat motor glider launched in 2000 by Rolladen Schneider Production ended after just 10 gliders were built when Rolladen Schneider went into receivership LS9 Role 18 metre class motorglider National origin Germany Manufacturer Rolladen Schneider First flight 1995 Number built 10 Contents 1 Development 2 Design 3 Specifications 4 See also 5 ReferencesDevelopment editThe LS9 was the sole self launching glider developed at Rolladen Schneider The prototype first flew in 1995 powered by a Rotax 535 two stroke engine Production of this engine was discontinued by Rotax putting the LS9 project on hold pending the development of a suitable engine The Solo 2625 engine and a Technoflug 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 Walter Binder Motorenbau GmbH having nearly 100 commonality with the Schempp Hirth Ventus CM installation Design editWings from the LS6 18w moulds with strengthened spars and leading edges Fuselage shape adapted from the LS4 by broadening the tail boom to accommodate the engine All new structure combining a new safety glass carbon cockpit with a full carbon composite fuselage behind the wing Empennage from the LS4 with new carbon and aramid composite construction Larger undercarriage 5 hub set further forward to prevent nose over with the engine at full power Innovative 210 mm x 65 mm steerable tailwheel integrated into the rudder directly under the hinge axis Single aerotow winching hook Carbon composite propeller mast deployed by electric screw jack system Engine recessed into the fuselage with electric starter fuel and coolant pumps Drive belt transmission to the large propeller Stall warning system activated during powered flight Specifications editGeneral characteristics Crew One Length 6 84 m 22 ft 5 in Wingspan 18 00 m 59 ft 1 in Height 1 43 m 4 ft 8 in Wing area 11 4 m2 123 sq ft Aspect ratio 28 4 Empty weight 350 kg 770 lb Gross weight 525 kg 1 155 lb Powerplant 1 Solo 2625 41 kW 55 hp Performance Maximum speed 270 km h 170 mph 150 kn Range 550 km 340 mi 300 nmi Maximum glide ratio gt 47 Rate of climb 4 0 m s 780 ft min Rate of sink 0 58 m s 114 ft min See also editRelated lists List of glidersReferences edit nbsp Wikimedia Commons has media related to Rolladen Schneider LS9 LS Flugzeugbau website Newsletter of the Auxiliary Powered Sailplane Association Website of LS dealer Solaire Canada Thomas F Fundamentals of Sailplane Design College Park Press 1999 Ewald J Flight Test of the LS 9 Sailplane and Gliding Oct 2000 Retrieved from https en wikipedia org w index php title Rolladen Schneider LS9 amp oldid 1083408516, wikipedia, wiki, book, books, library,
