All Figures

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f1.eps} \end{figure}$ Figure 1: Projections of impact points onto the asteroid equatorial plane. Period of rotation is equal to 1.1 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

In the text

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f2.eps} \end{figure}$ Figure 2: Projections of impact points onto the asteroid equatorial plane. Period of rotation is equal to 1.1 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

In the text

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f3.eps} \end{figure}$ Figure 3: Projections of points of possible erosion onto the asteroid equatorial plane. Rotation period is of 1.1 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

In the text

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f4.eps} \end{figure}$ Figure 4: Projections of points of possible erosion onto the equatorial plane of asteroid. Rotation period is of 1.1 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

In the text

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f5.eps} \end{figure}$ Figure 5: Projections of points of possible erosion onto the equatorial plane of asteroid. Rotation period is of 4.63 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

In the text

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f6.eps} \end{figure}$ Figure 6: Projections of points of possible erosion onto the equatorial plane of a sphere asteroid for the case of a clean solid surface. Rotation period is of 1.1 hour. Viewing the asteroid looking down on the north pole.
Open with DEXTER

In the text

$\begin{figure} \par\includegraphics[width=8.6cm,clip]{m2333f7.eps} \end{figure}$ Figure 7: The fraction of the total number of impacting particles fallingon to the leading sides of the asteroid depending on the asteroid rotation period. Particles initially are distributed uniformly inside a spherical layer 200 to 1000 ${\rm km}$ from the asteroid center. The followingmodels of gravitational attraction of particles are considered (from the upper curve to the lower one): (1) the asteroid of triaxial ellipsoid shape with the semiaxes 28, 12, 10.5 ${\rm km}$ attracts like a sphere of the same mass; (2) the asteroid has the triaxial ellipsoid shape above and its potential is expressed by Eq. (1); (3) the asteroid of the same mass has dumb-bell shape and its potential expressed by Eq. (4).
Open with DEXTER

In the text

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f8.eps} \end{figure}$ Figure 8: Combined contribution to the angular momentum of the asteroid from all impacting particles via the asteroid rotation period: for the asteroid of triaxial ellipsoid shape with semi-axes 28, 12, 10 ${\rm km}$ (circles) and for a dumb-bell shaped asteroid of the same mass (open triangles).
Open with DEXTER

In the text

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f1.eps} \end{figure}$	Figure 1: Projections of impact points onto the asteroid equatorial plane. Period of rotation is equal to 1.1 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f2.eps} \end{figure}$	Figure 2: Projections of impact points onto the asteroid equatorial plane. Period of rotation is equal to 1.1 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f3.eps} \end{figure}$	Figure 3: Projections of points of possible erosion onto the asteroid equatorial plane. Rotation period is of 1.1 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f4.eps} \end{figure}$	Figure 4: Projections of points of possible erosion onto the equatorial plane of asteroid. Rotation period is of 1.1 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f5.eps} \end{figure}$	Figure 5: Projections of points of possible erosion onto the equatorial plane of asteroid. Rotation period is of 4.63 hour. Viewing the asteroid looking down on the north pole. Trailing sides are at the left upper and right lower quarters of the picture.
Open with DEXTER

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f6.eps} \end{figure}$	Figure 6: Projections of points of possible erosion onto the equatorial plane of a sphere asteroid for the case of a clean solid surface. Rotation period is of 1.1 hour. Viewing the asteroid looking down on the north pole.
Open with DEXTER

$\begin{figure} \par\includegraphics[width=8.8cm,clip]{m2333f8.eps} \end{figure}$	Figure 8: Combined contribution to the angular momentum of the asteroid from all impacting particles via the asteroid rotation period: for the asteroid of triaxial ellipsoid shape with semi-axes 28, 12, 10 ${\rm km}$ (circles) and for a dumb-bell shaped asteroid of the same mass (open triangles).
Open with DEXTER