| Specifications |
| wing span |
325 cm |
| wing airfoil section |
NACA-4412 |
| wing area |
1.76m2 |
| canard span |
168.8 cm |
| canard area |
0.35 m2 |
| canard airfoil section |
NACA-4412 |
| vertical fin |
NACA-0012 |
| Length overall |
288 cm |
| Height overall |
90.88 cm |
| Body diameter |
25 cm |
| propeller Diameter |
61 cm |
| Max. launching weight |
83 kg |
| Max. payload weight |
40 kg |
| Launching speed |
64 Knots |
| Cruise speed |
165 Knots |
| Endurance |
1.5 h (Can be increased) |
| Engine Type |
WAE-342 |
| No. of cylinders |
2 |
| Engine volume |
342 cc |
| Max. power |
25 hp |
| Max. RPM (with propeller installed) |
7000-7500 |
| Weight |
8.5 kg |
| Fuel type |
Mixture of oil and Benzene |
| ceiling |
8000-10000 ft |
| Max. Thrust |
65-70 lb |
| Fuel tank capacity |
17 lit |
| Engine Type |
Vanckle Engine P73 rotary engine |
| Engine volume |
208 cc chamber size |
| Max.power |
30 hp |
| Max. RPM |
8000-8500 |
| Weight |
10 kg |
| Fuel type |
Mixture of oil and Benzene |
| Ceiling |
15000-17000 ft |
| Max. Thrust |
75-80 lb |
