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TeST s.r.o.

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

TST-6 DUO

tst_6_duo.jpg (76366 bytes)

 

Number of seats

 

2

Engine

 

Rotax 582

Span

m

14.6

Wing area

m2

12.9

Wing load

kg/m2

34.9

Airfoil

 

Wortmann FX 61-184

Aspect ratio

 

17.0

Length

m

6.4

Height

m

2.3

cockpit width

m

1.02

Empty weight

kg

265

Gross weight

kg

450

Vne

km/h

170

Max. cruising speed

km/h

150

Manoeuvring speed

km/h

120

Max. speed with extended air brakes

km/h

160

Stall speed

km/h

65

Economical cruising speed

km/h

90 -110

Tank volume

l

36

Economical fuel consumption

l/h

8

Take-off run

m

150

Take off over 50'

m

250

Landing run

m

150

Landing over 50'

m

350

Rate of climb

m/sec

3.5

Service ceiling

km

5

Glide ratio

 

16 / 100

Min. sinking rate

m/sec

2

design criteria

 

UL - 2

G - loads

 

+4 / -2