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Hohmann Transfer Orbit (Δv1, Δv2 & Transfer Time) Calculator

Easily calculate and compute hohmann transfer orbit (δv1, δv2 & transfer time) calculator with accurate equations, live formulas, and expert guidance.

E.g., Low Earth Orbit (LEO) ~300 km.

E.g., Geostationary Earth Orbit (GEO) = 35,786 km.

Calculated Result
3.89 km/s

Total Transfer Δv

Total Transfer Δv

3.89 km/s

Total Transfer Delta V Km Per Sec

3.893

First Burn Delta V1 Km Per Sec

2.426

Second Burn Delta V2 Km Per Sec

1.467

One Way Transfer Time Hours

5.28

3.89 — km/s

Calculation Breakdown

  1. Applied FormulaComputes the minimum two-impulse orbital maneuver delta-v burns (perigee insertion and apogee circularization) and flight duration between two coplanar circular orbits.\Delta v_{\text{total}} = \sqrt{\frac{\mu}{r_1}}\left(\sqrt{\frac{2r_2}{r_1+r_2}} - 1\right) + \sqrt{\frac{\mu}{r_2}}\left(1 - \sqrt{\frac{2r_1}{r_1+r_2}}\right)

Hohmann Transfer Orbit Metric Output

Interactive visualization based on your current inputs

Calculated Value
0.01.01.92.93.9Total Transfer Δv

What Is the Hohmann Transfer Orbit (Δv1, Δv2 & Transfer Time) Calculator?

This tool computes hohmann transfer orbit (δv1, δv2 & transfer time) calculator with high precision arithmetic.

How Does the Hohmann Transfer Orbit (Δv1, Δv2 & Transfer Time) Calculator Work?

Computes the minimum two-impulse orbital maneuver delta-v burns (perigee insertion and apogee circularization) and flight duration between two coplanar circular orbits.

Hohmann Transfer Orbit (Δv1, Δv2 & Transfer Time) Calculator Formula & Variables

The core mathematical equation utilized by this calculator is expressed as:

Δvtotal=μr1(2r2r1+r2−1)+μr2(1−2r1r1+r2)\Delta v_{\text{total}} = \sqrt{\frac{\mu}{r_1}}\left(\sqrt{\frac{2r_2}{r_1+r_2}} - 1\right) + \sqrt{\frac{\mu}{r_2}}\left(1 - \sqrt{\frac{2r_1}{r_1+r_2}}\right)

Computes the minimum two-impulse orbital maneuver delta-v burns (perigee insertion and apogee circularization) and flight duration between two coplanar circular orbits.

How to Use the Hohmann Transfer Orbit (Δv1, Δv2 & Transfer Time) Calculator

  1. Enter your parameters into the designated input fields to calculate the result immediately.

Step-by-Step Example Calculation

Hohmann Transfer Orbit (Δv1, Δv2 & Transfer Time) Calculator Example

Input Values:

initialOrbitAltitudeKm:300
finalOrbitAltitudeKm:35786
Worked Steps: Sample evaluation based on standard reference conditions.

Understanding Your Result

The calculated primary figure indicates the optimal or required km/s.

Factors That Affect the Result

  • Measurement tolerances, operational variance, and real-world conditions.

When Should You Use This Calculator?

  • Everyday budgeting, technical homework, professional estimation, and household projects.

Assumptions & Limitations

  • Assumes standard atmospheric or environmental parameters unless specified.

Frequently Asked Questions

Calculation Accuracy & Reference Note

Double-precision IEEE 754 arithmetic with validated empirical constants.

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