Eta Aircraft eta
- Eta Aircraft eta
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The eta is a German-Italian Open Class two-seater flapped self-launching
glider manufactured byETA Aircraft . It is the highest performing glider [http://www.daec.de/se/downfiles/2008/DMSt-WO2008.pdf Handicap list 2008] of theDeutscher Aero Club - accessed 2008-08-07] .On
July 31 ,2000 at 13:19 (in Cochstedt, Germany) the eta made its first flight making 2meter s of height, the second flight was the first aerotow take off flight to reach 1500 metres was at 13:58. The third flight was self powered and had no problems. The official presentation was onAugust 1 .Three etas have been manufactured to date. The second prototype was extensively damaged in 2003 during the spin tests required for the type certification. Both pilots parachuted to safety. The prototype was repaired and the tests completed successfully.
The glider will be produced by hand in a small series, at a rate of about three per year.
Eta is an example of a current trend in glider development in which private pilots initiate the development of new open class gliders. Currently, the private development of the Concordia sailplane promises a further elevation of lift-drag (l/D) ratio of several points.
Eta participated in a World Championship for the first time in 2003 at
Leszno . The pilotJanusz Centka was able to win five days and achieved an overall second place. Good placings have also been achieved by eta in later competitions. The glider is however hampered by the current weight limitation in the Open Class, which does not allow it to fly with a sufficiently high wingloading in strong weather, to the advantage of its opponents.pecifications (variant)
aerospecs
ref=
met or eng?= metcrew=Two
capacity=
length m=9.84
length ft=32
length in=3
span m=30.90
span ft=101
span in=5
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=
height ft=
height in=
wing area sqm=18.6
wing area sqft=200
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio= 51.3
empty weight kg=600
empty weight lb=1,320
gross weight kg=850
gross weight lb=1,870
lift kg=
lift lb=eng1 number=1
eng1 type=Solo 2625
eng1 kw= 47
eng1 hp= 63
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=max speed kmh=280
max speed mph=175
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio= 72
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=armament1=
armament2=
armament3=
armament4=
armament5=
armament6= aircontent
see also=
related=
similar aircraft=
lists=References
* [http://www.eta-aircraft.de/ ETA-Aircraft webpage]
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