Mars transfer orbit

A heliocentric orbit (also called circumsolar orbit) is an orbit around the barycenter of the Solar System, which is usually located within or very near the surface of the Sun. All planets, comets, and asteroids in the Solar System are in such orbits, as are many artificial probes and pieces of debris. The moons of planets in the Solar System, by contrast, are not in heliocentric orbits as they orbit their respective planet.

The barycenter of the Solar System, while always very near the Sun, moves through space as time passes depending on where other large bodies in the Solar System, such as Jupiter and other large gas planets, are located at that time. A similar phenomenon allows the detection of exoplanets by way of the radial velocity method.

The helio- prefix is derived from the Greek word helios, meaning "sun", and also Helios, the personification of the Sun in Greek mythology.

The first spacecraft to be put in a heliocentric orbit is Luna 1, which was planned to impact the Moon but instead missed due to an incorrectly timed upper stage burn.

A trans-Mars injection (TMI) is a heliocentric orbit in which a propulsive maneuver is used to set a spacecraft on a trajectory, also known as Mars transfer orbit, which will cause it to arrive at Mars.

Every two years, low-energy transfer windows open up which allow movement between planets with the lowest possible delta-v requirements. Transfer injections can place spacecraft into either a Hohmann transfer orbit or bi-elliptic transfer orbit. Trans-Mars injections can be either a single maneuver burn, such as that used by the NASA MAVEN orbiter, or a series of perigee kicks, such as that used by the ISRO Mars Orbiter Mission.

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