Hohmann Transfer Equation:
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A Hohmann transfer is an orbital maneuver that moves a spacecraft between two circular orbits in the same plane using two engine impulses. It is the most fuel-efficient method for such transfers.
The calculator uses the Hohmann transfer equations:
Where:
Explanation: The first burn transfers the spacecraft to an elliptical transfer orbit, and the second burn circularizes the orbit at the new altitude.
Details: Hohmann transfers are fundamental to space mission planning, used for satellite deployments, interplanetary trajectories, and space station rendezvous.
Tips: Enter both orbit radii in kilometers. For Earth orbits, the default μ value of 398600 km³/s² is appropriate. For other bodies, use their specific μ values.
Q1: When is a Hohmann transfer not optimal?
A: For very large orbit changes (radius ratio > 11.94), bi-elliptic transfers may be more efficient.
Q2: How does plane change affect Δv requirements?
A: This calculator assumes coplanar orbits. Plane changes require additional Δv not accounted for here.
Q3: What are typical Δv values for Earth orbits?
A: LEO to GEO transfer typically requires about 4 km/s total Δv.
Q4: How accurate is this calculator?
A: It provides theoretical minimum Δv. Real missions require additional margins for perturbations and control.
Q5: Can this be used for interplanetary transfers?
A: The basic principle applies, but interplanetary transfers typically use patched conic approximations.