Masatoshi Hirabayashi,
Masatoshi (Assistant Professor, Department of Aerospace Engineering, Auburn University, USA) Hirabayashi,
Yuichi Tsuda
Elsevier Science
e druk, 2022
9780323997317
Hayabusa2 Asteroid Sample Return Mission
Technological Innovation and Advances
Specificaties
Paperback, blz.
|
Engels
Elsevier Science |
2022
ISBN13: 9780323997317
Rubricering
Levertijd ongeveer 9 werkdagen
Gratis verzonden
Samenvatting
Hayabusa2 Asteroid Sample Return Mission: Technological Innovation and Advances covers the second Japanese asteroid sample return mission. The purpose of the mission is to survey the asteroid Ryugu’s surface features, touch down on the asteroid, form an artificial crater by shooting an impactor, and collect sample materials. This book covers these operations, along with everything known about key technologies, hardware and ground systems upon Hayabusa2’s return to Earth in 2020. This book is the definitive reference on the mission and provides space and planetary scientists with information on established technologies to further advance the knowledge and technologies in future space exploration missions.
Specificaties
Inhoudsopgave
1. Introduction Tsuda, M. Yoshikawa, Hirabayashi, Kikuchi Summary of this book<br>2. Mission objectives Tsuda, M. Yoshikawa <br>3. Cruise and approach phases Tsuda, Saiki <br>4. Asteroid-proximity phase Tsuda, Saiki <br>5. Re-entry phase Tsuda, Saiki, Nakazawa Including the collection of the sample capsule<br>6. Operation planning and execution 6 Station-keeping (HPNAV) Takei, Keep the spacecraft at the home position.<br>7. Controlled descent (GCP-NAV) Ono, Ogawa Descent for special operations. Ground Control Point Navigation<br>8. Observation campaign Takei, Operations for Box-A, B, C, Mid-alt, DO, CRA1, 2.<br>9. TD (6DoF control) Terui Touchdown planning and results<br>10. TMT Ogawa Image processing <br>11. MASCOT Mimasu Separation of MASCOT, and interface between JAXA and DLR/CNES<br>12. MINERVA-II-1, 2 K. Yoshikawa, van Wal. MINERVA-II-1 separation operation and landing site operation<br>13. SCI Saiki, Mimasu <br>14. Solar conjunction phase Soldini <br>15. Fault management Takei, <br>16. Spacecraft dynamics, orbit determination, and trajectory design 16 Gravity/Radiometric science Ikeda, Takeuchi Gravity measurement<br>17. IES trajectory design Tsuda Low-thrust trajectory design and approach trajectory design<br>18. Orbit determination Takeuchi Orbit determination during Regular and Special Operation; Optical Navigation Phase, DDOR. <br>19. Contact dynamics K. Yoshikawa Spacecraft dynamics during the touchdown operation, especially during the contact.<br>20. MINERVA/TM orbit design Ooki, K. Yoshikawa, Ikeda Orbit design for MINERVA-II-2, and its dynamics<br>21. Quasi-periodic orbit Kikuchi Searching for orbits that the spacecraft can stay around the body. <br>Hardware systems developments<br>22. Sampler Sawada, K. Yoshikawa <br>23. IES Nishiyama, Hosoda, Tsukizaki Ion Engine System<br>24. Power system Shimada <br>25. Thermal design Nakazawa Thermal design and analysis; thermal analysis for the touchdown operation<br>26. AOCS AOCS <br>27. Communication subsystem Toda, Takei <br>28. RCS Mori <br>29. LIDAR, LRF Terui <br>30. CAM-H, DCAM Sawada <br>31. Sample-return capsule Yamada, Nakazawa Return capsule design<br>32. Ground station Fujii, Takeuchi Communication operation using the Usuda station and DSN. <br>33. HIL (operation training) Takei Operation training<br>34. Data archive (SPICE) Yamamoto Hayabusa2 mission and beyond<br>35. Outreach activity M. Yoshikawa <br>36. Industrial effort NEC <br>37. Extended mission Mimasu, Hirabayashi, at al Extended mission of the Hayabusa2 mission