DOE design variables table
| Case | TOFL (ft) | Cruise Speed (kt) | Rate of climb (fpm) | Stall speed (kt) | Flying range (nm) | Cruise altitude (ft) |
|---|---|---|---|---|---|---|
| MIN | 1,100 | 70 | 300 | 43 | 150 | 6,000 |
| MAX | 1,500 | 130 | 650 | 53 | 300 | 12,000 |
| 1 | 1,239 | 123 | 644 | 51.5 | 262 | 10,904 |
| 2 | 1,354 | 119 | 579 | 52.3 | 204 | 8,453 |
| 3 | 1,388 | 86 | 609 | 52.5 | 254 | 10,365 |
| 4 | 1,403 | 109 | 575 | 50.8 | 194 | 8,040 |
| ⋮ | ⋮ | ⋮ | ⋮ | ⋮ | ⋮ | ⋮ |
| 350 | 1,374 | 102 | 404 | 46.0 | 264 | 6,060 |
| TOFL (ft) | Cruise Speed (kt) | Rate of climb (fpm) | Stall speed (kt) | Flying range (nm) | Cruise altitude (ft) | |
|---|---|---|---|---|---|---|
| 1,100 | 70 | 300 | 43 | 150 | 6,000 | |
| 1,500 | 130 | 650 | 53 | 300 | 12,000 | |
| 1,239 | 123 | 644 | 51.5 | 262 | 10,904 | |
| 1,354 | 119 | 579 | 52.3 | 204 | 8,453 | |
| 1,388 | 86 | 609 | 52.5 | 254 | 10,365 | |
| 1,403 | 109 | 575 | 50.8 | 194 | 8,040 | |
| ⋮ | ⋮ | ⋮ | ⋮ | ⋮ | ⋮ | |
| 1,374 | 102 | 404 | 46.0 | 264 | 6,060 |
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