Missile Specifications
| |
Standard 201 |
300 Missile |
| Engine model |
Lycoming IO-360-A3B6D |
Continental IO-550-A |
| Horsepower |
200 hp |
300 hp |
| Propeller |
74" McCauley 2-blade |
75" Hartzell 3-blade |
| Max. takeoff weight |
2,740 lbs |
3,200 lbs |
| Max. landing weight |
2,740 lbs |
3,083 lbs |
| Standard empty weight |
1,760 lbs |
2,010 lbs |
| Max. useful load |
980 lbs |
1,190 lbs |
| Wing loading |
15.6 lbs/ft |
18.3 lbs/ft |
| Power loading |
13.7 lbs/hp |
10.7 lbs/hp |
| Stall speed |
60 kts |
61 kts |
| Service ceiling |
18,800 ft |
18,800 ft |
| Max. rate of climb |
1,080 ft/min |
1,550 ft/min |
| Max. level speed (kts) |
169 kts |
193 kts |
| Cruise speed (kts) 77.5% |
164 kts |
186 kts |
| Takeoff over 50 ft obstacle |
1,500 ft |
1,200 ft |
|
|
