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Hohmann second burn Δv calculator

Circularising at geostationary distance after a Hohmann transfer from a 6778000 m orbit around Earth takes a second burn of 1456.50088963 m/s. Enter μ for the central body and the inner and outer orbit radii to get that second delta-v. Free in your browser.

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If you enter
Gravitational parameter
398,600,441,800,000
Radius inner
6,778,000
Radius outer
42,164,000
You get
Delta v2
1,456.50088963 m/s

A Hohmann transfer is the classic two-impulse path between two coplanar circular orbits: the first burn places the craft on an elliptical transfer orbit whose periapsis and apoapsis touch the inner and outer circles, and the second burn circularises at the destination radius. Mission planners, homework checkers, and concept-study scripts often need only that second burn delta-v—the speed change at apoapsis that raises (or lowers) the periapsis until the orbit is circular again—without integrating a full trajectory suite.

What the second Hohmann burn does

A Hohmann transfer moves a craft between two circular orbits in the same plane with two burns. The first puts it on an ellipse whose closest and farthest points touch the inner and outer circles. When the craft reaches the far point of that ellipse, it is moving too slowly to stay on the outer circle, so a second burn adds the speed needed to make the orbit circular. This calculator returns only that second speed change, which is what many homework checks and concept studies ask for.

How it is worked out and what to watch for

The calculator takes the circular speed at the outer radius, the square root of μ divided by that radius, and multiplies it by one minus the square root of twice the inner radius over the sum of both radii. With Earth's μ, 6778000 m and 42164000 m, the result is 1456.50088963 m/s. The most common slip is entering altitudes instead of distances from the centre: add the body's radius first. Also keep μ and the radii in the same unit system.

Is radius altitude or distance from the center?

Both radii are distances from the central body's center of mass to the circular orbits. If you only know altitude, add the body radius first before calling the calculator.

How is this different from a rocket-equation or plane-change Δv tool?

This tool returns only the second impulsive burn of a coplanar Hohmann transfer between two circular orbits. Rocket-equation calculators map mass ratio and exhaust velocity to total Δv; plane-change tools combine two speeds with a turn angle via the law of cosines.

What is the second burn from low Earth orbit to geostationary distance?

With Earth's μ, an inner radius of 6778000 m and an outer radius of 42164000 m, the second burn is 1456.50088963 m/s. That is the classic circularisation step at the top of a transfer to geostationary distance.

What units does the result use?

With μ in cubic metres per second squared and both radii in metres, the second-burn delta-v comes out in metres per second. Keep both radii in the same unit system as μ, or the number will not mean anything.

Why is the second burn smaller between closer orbits?

Because the transfer ellipse is less elongated when the two circular radii are closer together, so less extra speed is needed at the far point of the ellipse to make the orbit circular again.

Everything on this page is available programmatically. This section is for teams who want to wire it into their own systems; everyone else can just use the tool above.

POSThttps://api.kit.forhosting.com/astro/hohmann-deltav2

Prefer to automate it? One authenticated POST creates the task; the result comes back by webhook or a signed link. The same capability also runs here on the web, by email and from Telegram — and soon from our app too.

curl -X POST https://api.kit.forhosting.com/astro/hohmann-deltav2 \
  -H "Authorization: Bearer $KIT_KEY" \
  -H "Content-Type: application/json" \
  -d '{"gravitational_parameter":398600441800000,"radius_inner":6778000,"radius_outer":42164000}'
{
  "gravitational_parameter": 398600441800000,
  "radius_inner": 6778000,
  "radius_outer": 42164000
}
{
  "task_id": "tsk_a1b2c3d4e5f6a1b2c3d4e5f6",
  "type": "astro.hohmann_deltav2",
  "status": "queued",
  "_links": {
    "result": "/tasks/tsk_…/result"
  }
}

The API is asynchronous: the call returns a task_id immediately and the result arrives by webhook. Polling is capped at 1 req/s per task.

Per request$0.002

Published price — no tokens, no invented credits. A failed task is never charged.

HTTPCodeMeaning
401unauthorizedMissing or invalid API key.
402insufficient_balanceYour balance doesn't cover the task price.
404unknown_typeThat task type doesn't exist.
429rate_limitedToo many requests. Use the webhook instead of polling.

No network, no random seed, and no wall clock—identical inputs always produce identical JSON.

What the Hohmann second burn is and how Δv2 is derived

Radius values are center-to-satellite distances, not altitudes above a surface—if you only know height, add the body radius first. The standard gravitational parameter mu equals G times central mass; with mu in cubic metres per second squared and radii in metres, delta-v two is in metres per second. Send gravitational_parameter as a finite strictly positive number—for example Earth mu near three point nine eight six times ten to the fourteen—and radius_inner plus radius_outer as finite strictly positive lengths in the same unit system.

Input contract, response shape, and non-positive radius errors

Example: Earth mu with an inner low-Earth scale radius near six point seven seven eight times ten to the six metres and an outer geostationary-scale radius near four point two one six four times ten to the seven metres yields a second-burn magnitude of roughly one point four seven kilometres per second—the classic LEO-to-GEO circularisation scale. Example: the same mu with two closer circular radii yields a smaller second burn, as expected when the transfer ellipse is less eccentric. Pair the free in-browser Hohmann second burn calculator with your own conversion of altitude to geocentric radius when the source data only quotes height above a planetary surface. POST a JSON object with three required fields. gravitational_parameter must be a finite number strictly greater than zero; missing, empty, non-numeric, zero, or negative values fail with invalid_input naming the field. radius_inner must be a finite number strictly greater than zero; radius_outer must likewise be finite and strictly greater than zero. The explicit product rule is that either non-positive radius is invalid_input because the Hohmann second-burn formula divides by the radii under square roots and is undefined for a vanishing or inverted radius. On success the body echoes gravitational_parameter, radius_inner, and radius_outer rounded to twelve significant digits for stable goldens, reports delta_v2 with the same rounding, sets unit to the string m/s, method to hohmann_deltav2, and formula to the compact identity string so documentation and UI labels stay aligned with the physics. Validation failures are not billed; successful API items use the published prepaid base price of $0.002.

Where a Hohmann second-burn Δv API earns its keep

Classrooms and tutoring platforms use a Hohmann second burn delta-v calculator so learners can check the circularisation burn for arbitrary planetary parameters and radius pairs without sign or unit mistakes when rearranging vis-viva by hand. Exam-prep generators need a deterministic oracle that marks zero or negative radii as invalid rather than silently returning Infinity or NaN that a buggy grader might treat as success. Early mission concept tools compare second-burn budgets across candidate outer targets—medium Earth orbits, geostationary radius, lunar-distance scales, and Martian circular paths—without installing Orekit, GMAT, or a local MATLAB toolbox.

Homework and exam verification

Students and graders compute Hohmann Δv2 for a given gravitational parameter and two circular radii, confirm SI units yield m/s, and get a clear invalid_input error when either radius is zero or negative by mistake.

Tutoring and curriculum generators

Lesson builders produce worked Hohmann circularisation examples with structured JSON for flashcards, step sheets, and auto-graded orbital-mechanics drills without embedding a full astrodynamics library.

Early mission concept sketches

Lightweight pipelines that need a stable outer-orbit circularisation burn from μ, r1, and r2 call a prepaid endpoint instead of reimplementing the Hohmann second-burn identity in every language for LEO–GEO and planetary comparisons.

How do I calculate the Hohmann second burn delta-v?

Send JSON with gravitational_parameter (μ, positive), radius_inner (r1, strictly positive), and radius_outer (r2, strictly positive). The response includes delta_v2 equal to |√(μ/r2)·(1 − √(2 r1/(r1+r2)))| and unit m/s for SI inputs.

What happens if either radius is zero or negative?

The request fails with invalid_input. Non-positive radius_inner or radius_outer is rejected because the Hohmann second-burn formula divides by the radii under square roots and is undefined for a vanishing or inverted radius.

What does the Hohmann second burn calculator cost?

The browser tool is free. API requests use prepaid KIT balance at $0.002 per successful call; invalid input is not billed.

Read the full KIT documentation →