STEMME S6 User Manual

Flight Manual STEMME S6
Doc.-No.:P400-006.000 E Page: 1-5 Revision: 2
Date of Issue: 07. October 2008 Date of Rev.: 20.05.2011
1.4 Dimensions and Specifications _____________________
Specifications
Fuselage Design Front section: carbon-fiber composites
Mid-section: steel-tube framework with
glass-fiber composite fairing
Rear section with integrated vertical
fin: carbon-fiber composites
Length
27.95 ft / 8.52 m
Height
8.04 ft / 2.45 m
Width
3.97 ft / 1.21 m
Wings Design
threepart,
Spar: carbon-fiber composites
Shell: carbon-fiber composites
sandwich-structure
Span
59.05 ft / 18.00 m
Wing Area
187.51 ft²/ 17.42 m²
Aspect Ratio
18.62
Dihedral
2°
Wing Airfoil
DU (changes with wingspan)
Air-brakes Design Schempp-Hirth-style Air-brakes at
outer wing
Length
4.905 ft / 1.495 m
Horizontal
Stabilizer
Design Carbon-fiber composite bars and
sandwich-structure
Stabilizer Span
10.73 ft / 3.20 m
Stabilizer Area
18.73 ft² / 1.74 m²
Airfoil
DU
Masses Max. Take-off Mass
(MTOM)
1874 lbs / 850 kg
Max. Wing Loading
10 lbs/ft² / 48.79 kg/m²
Max. Weight of non-
lifting Parts
1367 lbs / 620 kg
Acceptable Range of
in-flight CG-Location
8.82 in to 16.10 in /
224 mm to 409 mm

STEMME S6 Specifications

General

Brand	STEMME
Model	S6
Category	Aircrafts
Language	English