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1. The spatial distribution of impact craters on Ryugu

2. Simultaneous geometric calibration and orbit-attitude determination of Hayabusa2’s deployable camera (DCAM3)

4. A dehydrated space-weathered skin cloaking the hydrated interior of Ryugu

5. A pristine record of outer Solar System materials from asteroid Ryugu’s returned sample

6. Site selection for the Hayabusa2 artificial cratering and subsurface material sampling on Ryugu

7. Preliminary analysis of the Hayabusa2 samples returned from C-type asteroid Ryugu

8. Hayabusa2 pinpoint touchdown near the artificial crater on Ryugu: Trajectory design and guidance performance

10. Hayabusa2’s kinetic impact experiment

11. Superior solar conjunction phase: Design and operations

12. Target markers for image-based autonomous navigation

13. Extended mission of Hayabusa2

15. Contributors

16. MASCOT lander release operation

17. Touchdown and sampling from asteroid Ryugu

18. Hayabusa2 radio science investigation

19. Overview of the Hayabusa2 asteroid proximity operations

20. Controlled descent of Hayabusa2 to Ryugu

22. Sensitivity degradation of optical navigation camera and attempts for dust removal

23. Chemical propulsion system

24. GNC design and results of Hayabusa2’s initial remote sensing operations

26. The MASCOT lander aboard Hayabusa2: The in-situ exploration of NEA (162173) Ryugu

27. Ballistic deployment of the Hayabusa2 artificial landmarks in the microgravity environment of Ryugu

31. Thermophysical properties of the surface of asteroid 162173 Ryugu: Infrared observations and thermal inertia mapping

33. The spatial distribution of impact craters on Ryugu

34. Hayabusa2’s station-keeping operation in the proximity of the asteroid Ryugu

36. Motion reconstruction of the small carry-on impactor aboard Hayabusa2

37. Hayabusa2’s superior solar conjunction mission operations: planning and post-operation results

40. Solar power sail mission of OKEANOS

45. Highly porous nature of a primitive asteroid revealed by thermal imaging

46. Alignment determination of the Hayabusa2 laser altimeter (LIDAR)

48. Hayabusa2 Landing Site Selection: Surface Topography of Ryugu and Touchdown Safety

49. Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data sets

50. Samples returned from the asteroid Ryugu are similar to Ivuna-type carbonaceous meteorites

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