Gravity turn

Gravity turn of the Space Shuttle

A gravity turn or zero-lift turn is a maneuver used in launching a spacecraft into, or descending from, an orbit around a celestial body such as a planet or a moon. It is a trajectory optimization that uses gravity to steer the vehicle onto its desired trajectory. It offers two main advantages over a trajectory controlled solely through the vehicle's own thrust. First, the thrust is not used to change the spacecraft's direction, so more of it is used to accelerate the vehicle into orbit. Second, and more importantly, during the initial ascent phase the vehicle can maintain low or even zero angle of attack. This minimizes transverse aerodynamic stress on the launch vehicle, allowing for a lighter launch vehicle.[1][2]

The term gravity turn can also refer to the use of a planet's gravity to change a spacecraft's direction in situations other than entering or leaving the orbit.[3] When used in this context, it is similar to a gravitational slingshot; the difference is that a gravitational slingshot often increases or decreases spacecraft velocity and changes direction, while the gravity turn only changes direction.

  1. ^ Glasstone, Samuel (1965). Sourcebook on the Space Sciences. D. Van Nostrand Company, Inc. pp. 209 or §4.97.
  2. ^ Callaway, David W. (March 2004). "Coplanar Air Launch with Gravity-Turn Launch Trajectories" (PDF). Masters Thesis. Archived from the original (PDF) on 2007-11-28.
  3. ^ Luidens, Roger W. (1964). "Mars Nonstop Round-Trip Trajectories". American Institute of Aeronautics and Astronautics. 2 (2): 368–370. Bibcode:1964AIAAJ...2..368L. doi:10.2514/3.2330. hdl:2060/19640008410.