Sizing Sensitivities (exchange rates)
| ΔOWE of 1% | ΔDrag of 1% | ΔSFC of 1% | |
|---|---|---|---|
| primary effect | |||
| blockfuel @ SPP design mission (150 PX, 2750 NM) | 0.70% | 1.01% | 1.18% |
| total fuel @ SPP design mission (150 PX, 2750 NM) | 0.72% | 0.98% | 1.16% |
| blockfuel @ SPP study mission (150 PX, 500 NM) | 0.42% | 0.63% | 1.07% |
| total fuel @ SPP study mission (150 PX, 500 NM) | 0.56% | 0.70% | 1.03% |
| ΔOWE of 1% | ΔDrag of 1% | ΔSFC of 1% | |
|---|---|---|---|
| new configuration | |||
| wing area | 0.95% | 0.28% | 0.34% |
| horizontal tail area | 1.45% | 0.43% | 0.53% |
| vertical tail area | 1.37% | 0.42% | 0.50% |
| T.O. Thrust per Engine @ S.L. | 0.95% | 0.29% | 0.34% |
| MTOW | 0.96% | 0.29% | 0.35% |
| MZFW | 0.97% | 0.08% | 0.10% |
| MLW | 0.82% | 0.25% | 0.30% |
| OWE | 1.43% | 0.12% | 0.14% |
| wing mass | 5.93% | 0.21% | 0.24% |
| fuselage mass | 0.00% | 0.00% | 0.00% |
| horizontal tail mass | 1.77% | 0.50% | 0.65% |
| vertical tail mass | 1.68% | 0.52% | 0.61% |
| landing gear mass | 1.01% | 0.31% | 0.37% |
| pylons mass | 0.52% | 0.16% | 0.19% |
| power unit mass | 0.57% | 0.17% | 0.21% |
| systems mass | 0.42% | 0.09% | 0.10% |
| furnishings mass | 0.05% | 0.00% | 0.01% |
| operator items mass | 0.02% | 0.01% | 0.01% |
| blockfuel @ SPP design mission (150 PX, 2750 NM) | 0.79% | 1.03% | 1.20% |
| total fuel @ SPP design mission (150 PX, 2750 NM) | 0.81% | 1.00% | 1.18% |
| blockfuel @ SPP study mission (150 PX, 500 NM) | 0.96% | 0.74% | 1.10% |
| total fuel @ SPP study mission (150 PX, 500 NM) | 0.90% | 0.80% | 1.07% |
| blockfuel @ MTOW mission (PL 17 to, 2500 NM) | 0.74% | 1.00% | 1.18% |
| total fuel @ MTOW mission (PL 17 to, 2500 NM) | 0.75% | 0.98% | 1.16% |