Using the Two-Burn Escape Maneuver for Fast Transfers in the Solar System and Beyond
Author(s) -
Robert B. Adams,
G. Richardson
Publication year - 2010
Publication title -
nasa sti repository (national aeronautics and space administration)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2010-6595
Subject(s) - mars exploration program , spacecraft , aerospace engineering , solar system , astrobiology , space exploration , solar sail , computer science , environmental science , physics , aeronautics , simulation , engineering
The two-burn maneuver to escape the gravitational pull of a central body is described. The maneuver, originally suggested by Hermann Oberth, improves efficiency considerably for a wide range of missions of interest in space exploration and scientific investigation. A clear delineation of when the maneuver is more effective is given, as are methods to extract the most advantage when using the maneuver. Some examples are given of how this maneuver can enable exploration of the outer solar system, near interstellar space, and crewed missions to Mars and beyond. The maneuver has the potential to halve the required infrastructure associated with a crewed mission to Mars and achieve increased solar escape velocities with existing spacecraft technologies.
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