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Delta-v calculator

Estimate ideal rocket delta-v from specific impulse or exhaust speed, and solve for either mass or the required propulsion performance.

Calculator

Ideal delta-v
2,079.44
Effective exhaust velocity
3,000
Specific impulse
305.915
Initial wet mass
10,000
Final mass
5,000
Propellant consumed
5,000
Wet/final mass ratio
2.00000000

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How this calculator works

Delta-v is the ideal change in velocity available from a burn, not the vehicle's final speed. Specific impulse is converted to effective exhaust velocity using standard gravity, 9.80665 m/s2. Initial mass includes propellant; final mass includes everything left after the burn. The single-stage model assumes constant effective exhaust velocity and excludes gravity, drag and steering losses.

Formula

delta-v = ve ln(m0/mf) = Isp g0 ln(m0/mf). m0 = mf exp(delta-v/ve); mf = m0 exp(-delta-v/ve); Isp = ve/g0.

Worked example

With effective exhaust speed 1000 m/s and a mass ratio of two, delta-v is 693.147 m/s. The same delta-v with 3 kg remaining requires an initial mass of 6 kg.

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Frequently asked questions

Is delta-v the same as speed?

It is a velocity-change budget. Gravity and the direction and timing of burns determine the resulting trajectory.

Which gravity converts specific impulse?

The conventional standard acceleration 9.80665 m/s2, even for a burn far from Earth.

Can wet and final masses be equal?

Yes, then no propellant is spent and ideal delta-v is zero. That case cannot determine a unique exhaust speed.

Sources

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