Abstract
We implement a numerical model to analyze the thermodynamics that can be used for navigation and orbit determination of future space missions to small bodies. Unlike past models that use a spherical homogeneous model, our model includes the real non-spherical shape of asteroid 433 Eros. The surface temperature map is expressed as a function of latitude and longitude directions for different initial isothermal temperatures. The lack of spherical symmetry is modeled along with the long and short term temperature variations as a consequence of the orbital and spin axis rotations of the body.
Original language | American English |
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State | Published - Feb 2013 |
Event | AAS/AIAA Spaceflight Mechanics Meeting - Kauai, HI Duration: Feb 1 2013 → … |
Conference
Conference | AAS/AIAA Spaceflight Mechanics Meeting |
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Period | 2/1/13 → … |
Keywords
- thermodynamics
- asteroids
- navigation
- space missions
Disciplines
- Aerospace Engineering
- Navigation, Guidance, Control and Dynamics