Evaluation of the Dynamic Environment of an Asteroid: Applications to 433 Eros
By Daniel J. Scheeres, B. Williams, J. Miller. 2000
225 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Astronomy and Astrophysics
View Paper: https://www.semanticscholar.org/paper/50a9bf90ab5239e4318f5c2dd5d184218f56a6cb
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In Aerospace Engineering
In Astronomy and Astrophysics
Citations in the corpus
- Orbit Mechanics About Asteroids and Comets (2012, background): “It has been demonstrated previously that it is the second-degree and -order gravity field terms that dominate the orbital stability for close-proximitymotion to uniformly rotating asteroids [2–6] and that SRP can destabilize spacecraft motion about a small body [7–10].”
- Determination of Shape, Gravity, and Rotational State of Asteroid 433 Eros (2002, background): “It should be noted that any surface ejecta that escapes the Roche lobe may initially be in orbit about Eros but would eventually be ejected from the asteroid into a heliocentric orbit due to interactions between the orbiting particle and the Eros gravity field (Scheeres et al. 2000).”