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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* 1000 lbs (454 kg)
Gross Weight 1550 lbs (704.5 kg)
Payload 550 lbs (220 kg)
Full Fuel Payload 391 lbs (177.7 kg)
Fuel Capacity 26.5 US gal (100.7 l)

* Typical empty weight is about 1100 lbs (500 kg)

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)

** Based on 125 HP prototype