The Wayback Machine - https://web.archive.org/web/20170404192742/http://www.rocketengineering.com:80/content/rocket-specifications
| |
Standard 231 |
305 Rocket |
| Engine model |
Continental TSIO-360-GB |
Continental TSIO-520-NB |
| Horsepower |
210 hp |
305 hp |
| Propeller |
74" McCauley 2-blade |
76.5" McCauley 3-blade |
| Max. takeoff weight |
2,900 lbs |
3,200 lbs |
| Max. landing weight |
2,900 lbs |
3,040 lbs |
| Standard empty weight |
1,860 lbs |
2,068 lbs |
| Max. useful load |
1,040 lbs |
1,132 lbs |
| Wing loading |
16.6 lbs/ft |
19.15 lbs/ft |
| Power loading |
13.8 lbs/hp |
10.5 lbs/hp |
| Stall speed |
60 kts |
61 kts |
| Service ceiling |
24,000 ft |
24,000 ft |
| Max. rate of climb |
1,080 ft/min |
1,550 ft/min |
| Max. level speed (kts) |
198 kts |
240 kts |
| Cruise speed (kts) 77.5% |
188 kts |
230 kts |
| Takeoff over 50 ft obstacle |
1,500 ft |
1,200 ft |