Main objectives achievable by hybrid-electric powertrain having baseline configuration as reference
| Mass variation | ICE mass | −20 ÷ −25% |
| Fuel mass for reference mission profile | −10 ÷ −15% | |
| Propulsion system mass | +25 ÷ +30% | |
| Take-off mass | ≈ −5% | |
| Performance variation | Climb duration | ≈ +10% |
| Minimum safety altitude | −45 ÷ −55% |
| ICE mass | −20 ÷ −25% | |
| Fuel mass for reference mission profile | −10 ÷ −15% | |
| Propulsion system mass | +25 ÷ +30% | |
| Take-off mass | ≈ −5% | |
| Climb duration | ≈ +10% | |
| Minimum safety altitude | −45 ÷ −55% |
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