Kerbal Space Program Delta V Calculator

🚀 Kerbal Space Program Delta V Calculator

Plan KSP stages with the Tsiolkovsky rocket equation, stock engine Isp presets, wet and dry mass, local gravity, target delta-v, reserve margin, TWR, and burn-time estimates.

🧭KSP Delta-v Presets
Stage math: delta-v uses wet mass, dry mass, and the selected pressure-adjusted Isp. The calculator also estimates TWR and burn time from stock KSP engine thrust and Isp data.
9.80665
KSP standard gravity g0
345 s
Selected stage Isp
2.00
Stage wet / dry ratio
Terrier
Engine preset loaded
Stage Inputs
Loads a common stock delta-v target while keeping the target editable.
Loads vacuum and sea-level thrust plus Isp for one active engine.
Use the stage mass before this stage burns.
Include tanks, engines, payload above the stage, and unusable propellant.
Vacuum is best for transfer stages; pressure mode blends sea-level and vacuum Isp.
0 for vacuum, 1 for Kerbin sea level, about 0.067 for Duna surface.
Stock engine vacuum Isp or your modded engine's vacuum value.
Used for launchers and pressure-adjusted estimates.
Clustered engines multiply thrust and mass flow, not rocket-equation delta-v.
Used for burn time and TWR estimates.
Pressure mode blends this with vacuum thrust for the selected atmosphere.
Use Kerbin 9.80665, Mun 1.63, Minmus 0.491, Duna 2.943, or your target body.
Compare against a maneuver, landing, ascent, or transfer budget.
Applied to calculated delta-v before judging mission margin.
Optional field used in the breakdown to show dry-mass payload share.
Repeats this stage delta-v for a quick asparagus or serial-stage estimate.
KSP Stage Result
Raw delta-v
0
m/s before reserve
Usable delta-v
0
m/s after selected reserve
Initial TWR
0.00
at local gravity
Burn time
0
seconds at full throttle
Rocket Equation Breakdown
Enter stage data and calculate.
💡Actionable KSP Delta-v Tips
Vacuum transfer stages: Use vacuum Isp for map-view burns, Mun returns, interplanetary cruisers, and high-altitude circularization. A Terrier, Poodle, or Nerv stage can look weak on TWR but still carry excellent delta-v.
Launch and landing stages: Delta-v alone is not enough near a surface. Check TWR against the local body because gravity losses grow when a stage burns slowly or cannot climb decisively.
Dry mass matters most: If a stage misses the target, reducing dead tankage or payload mass often adds more delta-v than adding another small tank that also increases wet mass.
Reserve discipline: Keep at least 5-15% for steering, inclination errors, capture corrections, and landing hover time. Nerv and ion craft often need extra burn-time patience, too.
📊Reference Tables
Stock Engine Delta-v Inputs
EngineRoleVac IspSea IspVac thrustSea thrustEngine mass
LV-T30 ReliantSimple lower stage310 s265 s240 kN205.16 kN1.25 t
LV-T45 SwivelSteerable early launcher320 s250 s215 kN167.97 kN1.50 t
LV-909 TerrierSmall vacuum lander345 s85 s60 kN14.78 kN0.50 t
48-7S SparkTiny probe or hopper320 s270 s20 kN16.56 kN0.13 t
RE-L10 PoodleMedium vacuum stage350 s90 s250 kN64.29 kN1.75 t
RE-M3 MainsailHeavy lifter core310 s285 s1500 kN1379.03 kN6.00 t
S3 KS-25x4 MammothVery heavy booster315 s295 s4000 kN3746.03 kN15.00 t
LV-N Nerv AtomicLong-range vacuum tug800 s185 s60 kN13.88 kN3.00 t
Use the custom engine option for modded parts, DLC balance changes, or part variants not shown here.
Common KSP Delta-v Budget Anchors
GoalTypical budgetBest Isp modeTWR noteReserve note
Kerbin surface to low orbitAbout 3400 m/sPressure to vacuum mixStart above 1.2 on KerbinAdd room for gravity turn errors
Low Kerbin orbit to Mun interceptAbout 860 m/sVacuumLow TWR is workableKeep capture correction margin
Mun landing from low orbitAbout 580 m/sVacuumHover-capable TWR helpsKeep landing hover fuel
Minmus landing from low orbitAbout 180 m/sVacuumVery low TWR can workReserve covers slope changes
Low Kerbin orbit to Duna interceptAbout 1060 m/sVacuumNerv burns can be longAdd correction and capture margin
Tylo land and return segmentHigh: 2200+ m/s each wayVacuumHigh TWR is vitalPlan generous descent reserve
These are planning anchors, not autopilot promises. Actual needs vary with ascent profile, payload, piloting, drag, and transfer window.
Formula and Unit Reference
MetricFormula usedKSP unit detailWhen to watch it
Delta-vIsp x 9.80665 x ln(wet / dry)Mass can be tonnes or kg if both masses matchEvery stage design
Mass ratioWet mass / dry massDry mass includes payload above this stageWhen adding tanks gives weak gains
Propellant fraction(wet - dry) / wetShown as a percent of wet stage massWhen comparing tank layouts
Mass flowTotal thrust / (Isp x 9.80665)kN divided by m/s gives tonnes per secondBurn-time planning
Initial TWRTotal thrust / (wet x local gravity)1 kN equals 1 t m/s2 in KSP-style unitsLaunches, landings, Tylo, Eve
Pressure IspSea Isp to vac Isp interpolationFirst-order estimate for 0-1 atmAtmospheric ascent estimates

You spend three hours in Vehicle Assembly Building. You put it all together carefuly, arrange the engines and tanks just so. Yes, that’s a good-looking rocket there. It has good symmetry. The parts is all there. Fire up the main engines. Flip the throttle switch. And then… crack! The rocket tear itself to pieces on the launch pad.

No, it wasn’t bad luck. It wasn’t some oddity of physics engine. The issue was failing to take rocket equation into account. In spaceflight, delta-v is the currency. Get out calculator and start tracking how much you’re spending.

Why Rockets Break and How to Fix Them

This is what I used to solve Tsiolkovsky rocket equation for me: According to the equation, your speed are proportional to exhaust velocity and mass of fuel divided by mass of empty rocket. Seems straightforward? Adding fuel adds weight, which require more fuel to lift, which adds even more weight. To get off the ground again, you’ll need another pound of fuel, which in turn means another pound of added weight. That’s where amateur rocket designer goes wrong, designing rockets that appear to be powerful but have no range.

Before committing yourself to any design, you must has an idea of how much fuel you can carry. There’s also a difference between transfer stage and launch stage. Atmospheric drag and gravity pull at you when you’re at Kerbin, trying to lift off. At that point, what you want is a lot of thrust for your weight. Use dense fuel. Use big engines.

Once you get up into space, where there’s no atmosphere, efficiency matter. This is where specific impulse, or Isp, can helps you out. High-Isp engines burns fuel slowly, but they put out more delta-v for every ton of propellant. The calculator has an option to switch back and forth between vacuum and sea-level Isp. All too often people thinks “engine = engine” and don’t differentiate between how different engines performs in different environments.

High mass reduces your delta-v. All that weight you have to haul around includes tanks, engines, and parts. It is dry mass. Too much dry mass? No matter how much fuel you add, you’ll lose. The mass ratio is calculated based off both your dry mass and your wet mass. Even an expensive engine won’t give you a good delta-v if your mass ratio are low. Frequently, it’s better to shave off some dry mass rather than adding some fuel tanks. Adding tanks will increase your wet mass.

Another important input is reserve margin. This is the engineering term for a safety buffer against unexpected actions or miscalculations. In space travel it’s the same thing. Should you calculate just enough delta-v to get to the Mun? A tiny steering mistake might strand you there forever. Ten to fifteen percent reserve isn’t pessimism. It’s survival. When the calculator calculates your total delta-v, it removes the reserve so that you know how much you can count on.

Get going fast with preset buttons. For example, they load common mission parameters such as Duna landings or Kerbin orbit insertion. It is not a solution but a starting point. The numbers depends on what engine you use, how much payload you carry, and how you pilot it. Take the presets to learn about the baseline requirement, and tweak to match your design.

Trade-offs are rocket science. High efficiency? High thrust? Rarely both. Heavy shielding? Low dry mass? Expect the math to penalize at least one of those choices. It’s not about maximizing all numbers. It’s about balancing them until the rocket flies.

You should of had patience and the right tools, and soon enough you won’t crash on the pad anymore. You’ll reach the stars. You’ll know that the engines cuts off in orbit with exactly the speed change you’d planned.

Kerbal Space Program Delta V Calculator

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