Rocket Potential Delta V

Delta V refers to the change in velocity required for a spacecraft to perform a particular maneuver, such as entering orbit around a planet or moon, or escaping from the gravitational pull of a celestial body. Use this calculator to test the potential delta v of a rocket.

mt
Save 8% of fuel for landing. Very rough estimate for the boostback burn, reentry burn, landing burn, and remaining fuel combined
Will this rocket have two stages?
Add a full tank of fuel to a 2nd stage in orbit. Greatly extends ΔV.
How massive is the first stage?
mt
How much fuel is in the first stage?
mt
Sea Level Specific Impulse.
s

3,236 m/s Exhaust Velocity (Ve)

Rocket mass is the mass of the rocket without fuel or payload.
mt
mt
How efficiently an engine creates thrust. Directly related to exhaust velocity.
s

3,432 m/s Exhaust Velocity (Ve)

Select a Common Rocket Engine to set example Specific Impulse

Specific Impulse values are estimates

Total ΔV8,966 m/s
Payload and Delta V (ΔV)Your RocketLEOMoonMars (Aerobrake)CeresVenus OrbitMercuryJupiterSaturnSun Escape05,00010,00015,00020,00025,00030,00035,00001020304050ΔV (m/s)Payload Mass (mt)
Delta VYour RocketLEOMoonMars (Aerobrake)CeresVenus OrbitMercuryJupiterSaturnSun Escape
29,2469,25614,91713,50018,96716,04625,42533,02627,18917,979
49,1739,25614,91713,50018,96716,04625,42533,02627,18917,979
69,1029,25614,91713,50018,96716,04625,42533,02627,18917,979
89,0339,25614,91713,50018,96716,04625,42533,02627,18917,979
108,9659,25614,91713,50018,96716,04625,42533,02627,18917,979
128,8999,25614,91713,50018,96716,04625,42533,02627,18917,979
148,8349,25614,91713,50018,96716,04625,42533,02627,18917,979
168,7719,25614,91713,50018,96716,04625,42533,02627,18917,979
208,6489,25614,91713,50018,96716,04625,42533,02627,18917,979
258,5029,25614,91713,50018,96716,04625,42533,02627,18917,979
308,3629,25614,91713,50018,96716,04625,42533,02627,18917,979
408,1029,25614,91713,50018,96716,04625,42533,02627,18917,979
507,8649,25614,91713,50018,96716,04625,42533,02627,18917,979