Calculate the static thrust of engines or propellers with the Static Thrust Calculator. Input airspeed, area, and pressure data for instant results.
Static Thrust Results
Mission ID/Description:
Engine Type:
Total Static Thrust:
Power Input:
Thrust-to-Power Ratio:
Static Thrust Performance Guide
| Propulsion Type | Typical Thrust (N) | Efficiency/Notes |
|---|---|---|
| Small Drone Propeller | 5–50 | η 0.65–0.8 |
| Aircraft Propeller | 500–5000 | η 0.75–0.9 |
| Turbojet (Small) | 1000–10000 | High mass flow |
| Turbofan (Commercial) | 100000–500000 | Optimized for cruise |
Note: Results are theoretical based on momentum theory (propeller) or jet thrust equations. Actual thrust depends on design and conditions. Consult aerospace engineers for precise analysis.
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