Technical Data and three dimensional side view of the DG-808C
Technical Data of DG-808C: |
|
|
|
span | m (ft) | 15 (49.2) | 18 (59.0) |
wing area | qm (sqft) | 10,68 (115.0) | 11,81 127.0) |
aspect ratio | / | 21,07 | 27,43 |
fuselage length | m (ft) | 7,055 (23.1) | 7,055 (23.1) |
fuselage height | m (ft) | 1,434 (4.7) | 1,434 (4.7) |
empty weight with parting (full instruments) | kg (lbs) | 334 (736) | 338 (745) |
empty weight no parting (full instruments) | kg (lbs) |
| 335 (738) |
wing loading with 80 kg payload | kg/qm (lbs/sqft) | 38,8 (7,95) | 35,1 (7,19) |
water ballast wings (option) | l (US gal) | 100 (26.4) | 100 (26.4) |
max. weight of the normal version | kg (lbs) | 525 (1156) | 525 (1156) |
max. wing loading | kg/qm (lbs/sqft) | 49,2 (10.1) | 44,5 (9,1) |
max. speed VNE | km/h (kn) | 270 (146) | 270 (146) |
stall speed with 80 kg (176 lbs) payload | km/h (kn) | 72 (39) | 68 (37) |
best glide ratio at max. weight about | / | 1:45 | 1:50 |
at speed | km/h (kn) | 116 (63) | 110 (59) |
min. sink at 400 kg (881 lbs) | m/s (ft/min) | 0,59 (116) | 0,50 (98) |
at speed | km/h (kn) | 80 (43) | 76 (41) |
|
|
|
|
Engine |
| SOLO 2625 |
|
power | KW/hp | 39/53 |
|
reduction gearing | / | 3:1 |
|
fuel tank fuselage | l (US gal.) | 22 (5.8) |
|
fuel tank wing (Option) | l (US gal.) | 2 x 10 (2x2,5) |
|
two stroke oil | / | Castrol Super TT |
|
fuel | / | Super 95 / 50:1 |
|
take-off distance 15m (50 ft) obst. weight 450 kg / 992 lbs) | m (ft) | ca. 200 (656) |
|
climb rate (weight 450 kg / 992 lbs) | m/s (ft/min) | 4,5 (885) |
|
Data power on for MSL and 15 Grad C.
Data for 18 m wingspan without winglets
With winglets the best glide ratio will increase approx. 1.5 points.
Short Description of DG-808c
Short description of the DG-808C and DG-808C Competition for printing
List of Spare DG-800
Drawings of the DG-808C
....and here you see another way of an independent take off.....
Art made by Mr. Waplinger, Soaring- and Tow Pilot
Other Articles of Interest: | |
| |
| |
| |
| |
| |
| |
| |