Rolladen-Schneider LS9

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LS9
Ls9 start.jpg
Role 18 metre-class motorglider
National origin Germany
Manufacturer Rolladen-Schneider
First flight 1995
Number built 10

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.

Development[]

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 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 , having nearly 100% commonality with the installation.

Design[]

  • 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.

Specifications[]

General 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: >47
  • Rate of climb: 4.0 m/s (780 ft/min)
  • Rate of sink: 0.58 m/s (114 ft/min)

References[]

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