Physics

Rocket Equation Calculator

Find delta-v from specific impulse and mass ratio.

Parameters Live Compute
Calculated Output
Delta-v 3,542.08
Exhaust velocity 2,942
Formula: Δv = Isp·g₀·ln(m₀ ÷ m_f)
Step-by-Step Breakdown
1. Values used:
2. Specific impulse = 300
3. Initial mass = 10,000
4. Final mass = 3,000
5.
6. Delta-v = 3,542.08
7. Exhaust velocity = 2,942
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The rocket equation links specific impulse and mass ratio to achievable delta-v.

The math behind it

Exhaust velocity v_e = Isp·g₀, then Δv = v_e·ln(m₀/m_f).

Worked Example

Isp 300 s, 10000 → 3000 kg → about 3543 m/s.

Frequently Asked Questions

What is specific impulse?

A measure of engine efficiency: exhaust velocity divided by g₀.

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