The orbit stability and insertion strategy around a small asteroid

1998 ◽  
Author(s):  
Jun'ichiro Kawaguchi ◽  
Shoji Yoshikawa
Keyword(s):  
Science ◽  
2020 ◽  
Vol 368 (6486) ◽  
pp. 67-71 ◽  
Author(s):  
M. Arakawa ◽  
T. Saiki ◽  
K. Wada ◽  
K. Ogawa ◽  
T. Kadono ◽  
...  

The Hayabusa2 spacecraft investigated the small asteroid Ryugu, which has a rubble-pile structure. We describe an impact experiment on Ryugu using Hayabusa2’s Small Carry-on Impactor. The impact produced an artificial crater with a diameter >10 meters, which has a semicircular shape, an elevated rim, and a central pit. Images of the impact and resulting ejecta were recorded by the Deployable CAMera 3 for >8 minutes, showing the growth of an ejecta curtain (the outer edge of the ejecta) and deposition of ejecta onto the surface. The ejecta curtain was asymmetric and heterogeneous and it never fully detached from the surface. The crater formed in the gravity-dominated regime; in other words, crater growth was limited by gravity not surface strength. We discuss implications for Ryugu’s surface age.


Icarus ◽  
2010 ◽  
Vol 210 (2) ◽  
pp. 707-712 ◽  
Author(s):  
M.J. Burchell ◽  
J. Leliwa-Kopystynski
Keyword(s):  

2005 ◽  
Vol 13 ◽  
pp. 738-742 ◽  
Author(s):  
M. Antonietta Barucci ◽  
Paolo D’Arrigo ◽  
P. Ball ◽  
Alain Doressoundiram ◽  
Elisabetta Dotto ◽  
...  

AbstractISHTAR (Internal Structure High-resolution Tomography by Asteroid Rendezvous) is a mission developed through ESA General Studies programme. The study, led by Astrium in cooperation with several scientific institutes throughout Europe, has produced a spacecraft design capable of performing multiple asteroid rendezvous and to characterize them with a focussed set of instruments. The ISHTAR concept is centred around a Radar Tomography paylod able to probe the internal structure of a small asteroid to depths of few hundred meters, combined with a small camera for investigation of the surface properties and a radio science experiment for gravity field measurement. This combination will allow the first detailed characterization of a NEO and will give valuable insights into the origin and evolution processes that govern the NEO population. In particular, ISHTAR will be able to visit at least 2 NEOs belonging to two different spectral classes, thereby allowing us to probe the diversity of the NEO population.


2021 ◽  
pp. 779-790
Author(s):  
J. G. HILLS ◽  
I. V. NEMCHINOV ◽  
S. P. POPOV ◽  
A. V. TETEREV
Keyword(s):  

Author(s):  
Jennifer N Larson ◽  
G Sarid

Abstract We introduce here our new approach to modeling particle cloud evolution off surface of small bodies (asteroids and comets), following the evolution of ejected particles requires dealing with various time and spatial scales, in an efficient, accurate and modular way. In order to improve computational efficiency and accuracy of such calculations, we created an N-body modeling package as an extension to the increasingly popular orbital dynamics N-body integrator Rebound. Our code is currently a stand-alone variant of the Rebound code and is aimed at advancing a comprehensive understanding of individual particle trajectories, external forcing, and interactions, at the scale which is otherwise overlooked by other modeling approaches. The package we developed – Rebound Ejecta Dynamics (RED) – is a Python-based implementation with no additional dependencies. It incorporates several major mechanisms that affect the evolution of particles in low-gravity environments and enables a more straightforward simulation of combined effects. We include variable size and velocity distributions, solar radiation pressure, ellipsoidal gravitational potential, binary or triple asteroid systems, and particle-particle interactions. In this paper, we present a sample of the RED package capabilities. These are applied to a small asteroid binary system (characterized following the Didymos/Dimorphos system, which is the target for NASA’s Double Asteroid Redirection Test mission).


Author(s):  
M. Hirabayashi ◽  
Y. Mimasu ◽  
N. Sakatani ◽  
S. Watanabe ◽  
Y. Tsuda ◽  
...  
Keyword(s):  

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