Flight Manual STEMME S 10 Date of Issue Oct. 1, 1990 page: 7
Amendment No.: -- Date: --
A4010013_08a-7/13.11.2015 14:34:00/14:34
1.4 Description and Technical Data
The STEMME S10 is a two-seat high performance motor glider with an innovative propulsion concept and
highly finished aerodynamic shape. The seats are arranged side-by-side (forward of the wing) and are
equipped with dual controls.
The wing is mounted to the fuselage in the upper third. It consists of an inner wing with flaps and Schempp-
Hirth air brakes and two outer wings with continuous ailerons.
The tailplane is designed as a "T"-type.
The two-wheel main landing gear can be retracted electrically and contains hydraulic brakes.
The engine is mounted in the fuselage in a central steel tubing frame near the aircraft's Center of Gravity.
Engine power is transmitted via a prop shaft made of composites and a reduction gearbox to the jointed
propeller in the fuselage nose. The propeller is folded in during soaring flight and covered by the movable
nose cone (propeller cone).
One fuel tank is placed in each of the two outer sections of the inner wing.
Technical data:
wingspan 75.5 ft 23.00 meters
length of fuselage 27.6 ft 8.42 m
height 5.74 ft 1.75 m
aspect ratio 28.22
wing area 201.64 sqft.
18.74 m
max. weight 1874 lb. 850 kg
max. wing loading 9.29 lb./sqft.
45.36 kg/m
airfoil HQ 41/14.35 (laminar profile)
mean aerodynamic wing chord 2.86 ft 0.873 m
engine Limbach L2400 EB1.AD
propeller STEMME 10AP-N
gear box ratio i = 1.18
To Next Page
Loading...
