Aspects of parking orbit selection in a manned Mars mission

Details Aspects of parking orbit selection in a manned Mars mission Aspects of parking orbit selection in a manned Mars mission

Dec 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992stin...9315367d&link_type=abstract

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Computer Science

Gravitational Effects, Manned Mars Missions, Parking Orbits, Precession, Structural Weight, Trajectory Optimization, Earth Orbits, Eccentricity, Inclination, Landing Sites

Scientific paper

For any round-trip Mars mission, the selection of a parking orbit at Mars must consider the precession caused by the oblateness of the planet. This precession will affect the departure condition for Earth return and, therefore, the initial mass required in low Earth orbit (LEO). In this investigation, which considers precession effects, minimum initial LEO masses were obtained for parking orbits characterized by having near-equatorial inclinations, high eccentricities, and three-dimensional departure burns (i.e., a burn with an in-plane and an out-of-plane velocity increment component). However, because near-equatorial inclination orbits have poor planetary coverage characteristics, they are not desirable from a science viewpoint. To enhance the potential for satisfying science requirements along with landing site accessibility, a penalty in the initial LEO mass is required. This study shows that there are a set of orbits characterized by low to moderate essentricities (e = 0.2 to 0.5) and nonequatorial inclinations (i = 70 to 140 deg) that reduce this initial LEO mass penalty. Therefore, careful selection of a parking orbit at Mars can enhance the potential for satisfying science requirements with minimal mass penalties.

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