Marquart Charger Specifications
All specifications are approximate, and will vary with individual aircraft. Always verify the specs of the particular plane in question. These numbers are given only as a general reference.
Physical
| Height | 7 ft 7 in (2.3 m) |
| Wingspan | 24 ft (7.3 m) |
| Length | 20 ft 8 in (6.3 m) |
| Wing Area | 170 ft2 (16 m2) |
| Wing Sweep | 10° |
| Airfoil | NACA 2412 |
| Design Empty Weight | 1100 lbs (499 kg) |
| Gross Weight | 1650 lbs (748.4 kg) |
| Payload | 550 lbs (220 kg) |
| Payload with Full Fuel | 391 lbs (177.7 kg) |
| Fuel Capacity | 26.5 US gal (100.7 l) |
Performance*
| Design Engine HP Range | 125-180 HP (93-134 kW) |
| Design Loading | +6/-4 G |
| Cruise Speed | 100 kt (115 mph) (185 km/h) |
| Stall Speed (Vs) | 37 kt (42 mph) (68 km/h) |
| Never-Exceed Speed (Vne) | 161 kt (185 mph) (298 km/h) |
| Best Glide Speed (Vg) | 65 kt (75 mph) (121 km/h) |
| Max Climb Rate at 1300 lbs | 1100 fpm (5.59 m/s) |
| Wing Loading | 9.12 lb/ft2 (0.385 kg/m2) |
| Power Loading | 12.4 lb/HP (7.57 kg/kW) |
| Range | 400+ miles (643+ km) |
* Based on 125 HP model