Use the Rocket Thrust Calculator to compute thrust based on mass flow rate and exhaust velocity. Ideal for students, engineers, and space enthusiasts.
Rocket Thrust Results
Mission ID/Description:
Environment:
Momentum Thrust:
Pressure Thrust:
Total Thrust:
Specific Impulse:
Rocket Performance Guide
| Rocket Type | Typical Thrust (kN) | Specific Impulse (s) |
|---|---|---|
| Solid Rocket | 100–5000 | 250–300 |
| Liquid Rocket (LOX/Kerosene) | 500–7000 | 300–350 |
| Liquid Rocket (LOX/LH2) | 500–2000 | 400–450 |
| Ion Thruster | 0.001–0.1 | 3000–9000 |
Note: Results are theoretical based on input parameters. Actual thrust depends on engine design, nozzle efficiency, and conditions. Consult aerospace engineers for precise performance analysis.
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