| Design Name: | P-5 |
| Designer: | Makarov A.V. |
| Design Date: | 05.02.2007 |
| File Name: | C:\Program Files\AirplanePDQ\P-5_2.dwg |
| Parameter | SI Units | User Units |
|---|---|---|
| Main Wing Span | 8.633 m | 8.633 m |
| Main Wing Chord (Root) | 1.659 m | 1.659 m |
| Main Wing Chord (Tip) | 0.6435 m | 0.6435 m |
| Main Wing Aspect Ratio | 7.499 | |
| Canard Span | 4. m | 4. m |
| Canard Chord (Root) | 0.5 m | 0.5 m |
| Canard Chord (Tip) | 0.5 m | 0.5 m |
| Canard Aspect Ratio | 8. | |
| Vertical Stabilizer Span | 1.401 m | 1.401 m |
| Vertical Stabilizer Chord (Root) | 0.5828 m | 0.5828 m |
| Vertical Stabilizer Chord (Tip) | 0.281 m | 0.281 m |
| Vertical Stabilizer Aspect Ratio | 1.622 | |
| naplyv Span | 1.966 m | 1.966 m |
| naplyv Chord (Root) | 3.371 m | 3.371 m |
| naplyv Chord (Tip) | 1.423 m | 1.423 m |
| naplyv Aspect Ratio | 0.8204 | |
| Max Fuselage Width | 1.006 m | 1.006 m |
| Max Fuselage Height | 1.287 m | 1.287 m |
| Fuselage Length | 4.894 m | 4.894 m |
| Tail Height above Ground | 2.554 m | 2.554 m |
| Wheel Track | 2.03 m | 2.03 m |
| Wheel Base | 3.843 m | 3.843 m |
| Propeller Diameter | 2. m | 2. m |
| Parameter | SI Units | User Units |
|---|---|---|
| Cabin Length | 1.27 m | 1.27 m |
| Cabin Max Width | 0.0 m | 0.0 m |
| Cabin Max Height | 1.232 m | 1.232 m |
| Parameter | SI Units | User Units |
|---|---|---|
| Main Wing Area, Gross | 9.938 m^2 | 9.938 m^2 |
| Flaps Area | 0.6151 m^2 | 0.6151 m^2 |
| Ailerons Area | 0.1671 m^2 | 0.1671 m^2 |
| Canard Area, Gross | 2. m^2 | 2. m^2 |
| Elevator Area | 0.6503 m^2 | 0.6503 m^2 |
| Vertical Stabilizer Area, Gross | 1.21 m^2 | 1.21 m^2 |
| Rudder Area | 0.5842 m^2 | 0.5842 m^2 |
| naplyv Area, Gross | 4.714 m^2 | 4.714 m^2 |
| Parameter | SI Units | User Units |
|---|---|---|
| Engine Model | VMKB M-14P(360 HP) | |
| Engine Power Rating | 2.685e+05 watts | 268.5 kW |
| Parameter | SI Units | User Units |
|---|---|---|
| Empty Weight | 692.7 kg | 692.7 kg |
| Gross Weight | 929.6 kg | 929.6 kg |
| Baggage Capacity | 22.68 kg | 22.68 kg |
| Payload with Max Fuel | 112.7 kg | 112.7 kg |
| Fuel Capacity | 0.177 m^3 | 177. liter |
| Max Wing Loading | 63.45 kg/m^2 | 63.45 kg/m^2 |
| Max Power Loading | 0.003463 kg/watts | 3.463 kg/kW |
| Number of Seats | 1 |
| Parameter | SI Units | User Units |
|---|---|---|
| Max Level Speed (0.0 m) | Outside analysis range. Increase target cruise speed to increase analysis speed range. | |
| Cruise Speed (0.0 m, 75.% Power) | Outside analysis range. Increase target cruise speed to increase analysis speed range. | |
| Stall Speed Clean (SL, Power On) | 27.4 m/s | 98.65 km/hr |
| Stall Speed 45. deg Flaps (SL, Power On) | 32.94 m/s | 118.6 km/hr |
| Max Rate of Climb (SL) | 17.8 m/s | 17.8 m/s |
| Max Lift to Drag Ratio (SL) | 18.77 |