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TeST s.r.o.

http://www.test.infoline.cz/

TST-3 ALPIN TM

Number of seats		1
Engine		Rotax 447
Span	m	13.8
Wing area	m^2	10.5
Wing load	kg/m^2	28.1
Airfoil		Wortmann FX 61-184
Aspect ratio		17.1
Length	m	5.9
Height	m	1.5
cockpit width	m	0.59
Empty weight	kg	140 / 195
Gross weight	kg	250 / 300
Vne	km/h	180
Max. cruising speed	km/h	165
Manoeuvring speed	km/h	130
Max. speed with extended air brakes	km/h	180
Stall speed	km/h	62
Economical cruising speed	km/h	90
Tank volume	l	15
Economical fuel consumption	l/h	5
Take-off run	m	200
Take off over 50'	m	350
Landing run	m	80
Landing over 50'	m	200
Rate of climb	m/sec	3
Service ceiling	km	3
Glide ratio		33 / 85
Min. sinking rate	m/sec	0.75
design criteria		JAR 22
G - loads		+5,2 / -2,6