| MitchellWing A-10 Motorglider |
|
| Specifications and Data |
| Feature | MitchellWing Owner's Manual A-10 (Orig. Release '98?) | Ameriplanes Website A-10D Zenoah G25B-1 equipped | 18 JLS - A-10 Factory built in 1984, S/N 123, w/ Zenoah G25B-1 |
| Wing Span - ft Wing Area - sq.ft Aspect Ratio Engine - Mfr _HP _Displacement - cc Empty Weight - lb Useful Load - lb Gross Weight - lb Wing Loading - lb/sq ft Design Stress - g's Pwr Loading - lb/hp Speeds - mph _Vne _Vmax _Vcr _Vstall - Pwr Off _Rotation Speed - mph _Maneuv. Speed - mph _Appr'ch Speed - mph Rate of Climb - ft/min _Best ROC Speed Rate of Sink - ft/min _Best ROS Speed Glide Ratio _Best L/D Speed Fuel Capacity - gal Range - 75% Pwr - gph _Hours - No Res. _Miles - No wind Takeoff - Wind calm _Ground Run - ft _Dist. 50' obs. - ft Landing - Wind calm _Ground Roll - ft _Dist. 50' obs. - ft Service Ceiling - ft |
34.33' 156 8.7 Zenoah (G25B-1?) 23 242 250 288 538 3.1? +6/-5.5 18.8? 63 63 58 27 32 50 40 650 40 240 35 16:1 40 3.0 1.25* 2.4* 140* 225 535 200 700 12,000 *Range and endurance values based on 1.25gph@75% are highly suspect. Fuel consumption is likely to be closer to 2.5 gal/hr, IMHO. JEC |
34.33' 136? 8.7 Zenoah G25B-1 22 242 270 280 550 3.5? +6/-5.5 18.8? 80 70 62 28 n/s n/s n/s 650 n/s 240 n/s 16:1 n/s 3.0 1.25* 2.4* 140* 250 600 250 750 12,000 *Ditto remarks offered in Owner's Manual column. JEC |
34.33' 156 8.7 Zenoah G25B-1 22 (manf.stated, prop?) 242 288 (as of 11/17) 240 (avg. flying) 518 (avg. w/5 gal fuel) 3.32 +4.6/-2.3 23.55 63? 63? 62? 28?tbd 32?tbd 50 40 650?tbd 40?tbd 240?tbd 35?tbd 16:1? 40?tbd 5.0 2.5?tbd 2.0?tbd 140?tbd 250?tbd 600?tbd 250?tbd 750?tbd 12,000?tbd ?tbd - Values for 18 JLS to be determined by actual measurement and/or analysis at a later date. JEC |
