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Hohmann Transfer Orbit

1925-01-01
  • Walter Hohmann
Spacecraft performing Hohmann transfer maneuver in astrodynamics.

(generated image for illustration only)

A Hohmann transfer is an orbital maneuver that moves a spacecraft between two coplanar circular orbits using two engine impulses. It is generally the most fuel-efficient two-burn maneuver. The transfer orbit is an ellipse that is tangential to both the initial and final orbits at its apoapsis and periapsis, requiring one burn to enter the ellipse and another to circularize.

The Hohmann transfer maneuver, described by Walter Hohmann in his 1925 book ‘The Attainability of Heavenly Bodies’, provides a baseline for efficient orbital transfers. The process begins with the spacecraft in a stable, circular orbit. The first burn, a prograde (in the direction of motion) impulse, is applied instantaneously. This adds energy to the orbit, changing it from a circle into an ellipse. The point of the burn becomes the periapsis (lowest point) of this new transfer ellipse, and its apoapsis (highest point) is designed to be tangential to the desired final circular orbit.

The spacecraft then coasts along this elliptical path, typically for half an orbital period. Upon reaching the apoapsis of the transfer ellipse, a second prograde burn is executed. This second impulse adds more energy, raising the periapsis of the orbit to match the apoapsis, thus circularizing the orbit at the new, higher altitude. While the Hohmann transfer is the most delta-v efficient for many scenarios, it is also time-consuming. For transfers where the ratio of the final to initial orbital radii is very large (greater than about 11.94), a bi-elliptic transfer can be more fuel-efficient, though it takes even longer.

UNESCO Nomenclature: 3301
– Aerospace engineering

Type

Abstract System

Disruption

Incremental

Usage

Widespread Use

Precursors

  • johannes kepler’s laws of planetary motion
  • isaac newton’s law of universal gravitation
  • the two-body problem solution in celestial mechanics

Applications

  • transferring satellites from low earth orbit (leo) to geostationary orbit (geo)
  • sending probes from earth’s orbit to mars’ orbit
  • planning rendezvous maneuvers for space stations
  • standard trajectory design for interplanetary missions

Patents:

NA

Potential Innovations Ideas

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Related to: hohmann transfer, orbital maneuver, astrodynamics, delta-v, fuel efficiency, elliptical orbit, apoapsis, periapsis, orbital mechanics, walter hohmann.

Historical Context

Hohmann Transfer Orbit

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(if date is unknown or not relevant, e.g. "fluid mechanics", a rounded estimation of its notable emergence is provided)

Related Invention, Innovation & Technical Principles

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