Stemme S6

(Redirected from Stemme S8)

The Stemme S6 is a two-seat touring motorglider manufactured by Stemme AG. Unlike the S10, the S6 has a non-retractable three-bladed propeller (that can feather like other touring motor gliders), a wider fuselage design, and tricycle landing gear, available both with fixed and retractable configurations. Its engine is a Bombardier-Rotax 914, the same engine used in the Stemme S10-VT.[2] The designers placed great importance on noise and vibration reduction.

Stemme S6
Role Touring motor glider
National origin Germany
Manufacturer Stemme AG
First flight 2006
Number built 18 by 2011[1]

The prototype S6 made its first flight on 29 November 2006 at Strausberg Airport, flown by Lothar Dalldorff. It received EASA approval on 22 October 2008.

Variants

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S6
100 hp, fixed landing gear.
S6-R
retractable landing gear.
S6-T
115 hp turbocharged engine
S6-RT
115 hp turbocharged engine, retractable landing gear. First flown 10 December 2002.[1]
S6ew Sky Sportster
20m wingspan with a 38 to 1 glide ratio[3]
S8-T
as S6-T
S8-RT
as S6-RT but with roomier cockpit and greater fuel capacity.

Specifications (S6-T)

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Data from Jane's All the World's Aircraft 2013-14.[1]

General characteristics

  • Crew: 1 pilot
  • Capacity: 1 passenger
  • Length: 8.52 m (27 ft 11 in)
  • Wingspan: 18.00 m (59 ft 1 in)
  • Height: 2.45 m (8 ft 0 in)
  • Wing area: 17.42 m2 (187.5 sq ft)
  • Aspect ratio: 18.6
  • Empty weight: 640 kg (1,411 lb)
  • Max takeoff weight: 850 kg (1,874 lb)
  • Powerplant: 1 × Rotax 914 F2 flat four, 84.5 kW (113.3 hp) geared drive
  • Propellers: 3-bladed MTV-7-A/170-51, 1.70 m (5 ft 7 in) diameter constant speed

Performance

  • Cruise speed: 256 km/h (159 mph, 138 kn) at FL100
  • Never exceed speed: 268 km/h (167 mph, 145 kn)
  • Range: 1,398 km (869 mi, 755 nmi) at FL160 with 130 litres of fuel, no reserve
  • Service ceiling: 4,875 m (15,994 ft) service
  • g limits: 5.3/-2.6
  • Maximum glide ratio: 36:1 for retractable, 30:1 for fixed, at 115 km/h (71 mph; 62 kn)
  • Rate of climb: 2.7 m/s (530 ft/min) maximum, at sea level
  • Rate of sink: 0.93 m/s (183 ft/min) minimum with 70 kg (154 lb) load
  • Wing loading: 48.79 kg/m2 (9.99 lb/sq ft)

References

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  1. ^ a b c Jackson, Paul A. (2013). Jane's All the World's Aircraft : development & production : 2013-14. IHS Global. pp. 280–1. ISBN 978-0-7106-3040-7.
  2. ^ Bayerl, Robby; Martin Berkemeier; et al.: World Directory of Leisure Aviation 2011-12, page 150. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  3. ^ "Stemme s6". Sport Aviation: 15. April 2014.
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