Computer model of Hayabusa 2 rendezvous with asteroid Ryugu
|Mission type||Asteroid sample return|
|Website||Hayabusa 2 on jaxa
|Launch mass||Total: 590 kg (1,300 lb)
MASCOT: 10 kg (22 lb)
MINERVA: 0.5 kg (1.1 lb)
|Dimensions||2 × 1.6 × 1.25 m (6.6 × 5.2 × 4.1 ft)|
|Start of mission|
|Launch date||3 December 2014, 04:22 UTC|
|Launch site||LA-Y, Tanegashima Space Center|
|End of mission|
|Landing date||December 2020 (planned)|
|Flyby of Earth|
|Closest approach||3 December 2015|
|Distance||3,090 km (1,920 mi)|
|(162173) Ryugu orbiter|
|Orbital insertion||June 2018 (planned)|
|Departed orbit||December 2019 (planned)|
The target is asteroid 162173 Ryugu (formerly designated 1999 JU3). Hayabusa 2 is expected to arrive at the target in July 2018, survey the asteroid for a year and a half, depart in December 2019, and return to Earth in December 2020.
The spacecraft features ion engines, upgraded guidance and navigation technology, antennas and attitude control systems. Operations at the asteroid will be similar[clarification needed] to those of the previous Hayabusa, but with an explosive device to dig the asteroid surface for fresh sample material.
Hayabusa 2 was approved by the Space Activities Commission, a board governing funding for the Japanese space program, during 2006. In July 2009, at the 27th ISTS (International Symposium on Space Technology and Science) conference in Japan, Makoto Yoshikawa of JAXA presented a proposal entitled "Hayabusa Follow-on Asteroid Sample Return Missions." In August 2010, JAXA obtained approval from the Japanese government to begin development of Hayabusa 2. The estimated cost of the project is 16.4 billion yen.
The German Aerospace Center built a small lander called MASCOT (Mobile Asteroid Surface Scout) for the mission in a cooperation with the French space agency CNES. The MASCOT carries an infrared spectrometer, a magnetometer, a radiometer and a camera, and is capable of lifting off of the asteroid to reposition itself for further measurements.
The Small Carry-on Impactor (SCI) is a small drop-off explosively formed penetrator, consisting of a 2.5 kilogram (5.5 lb) copper projectile and a 4.5 kilogram (10 lb) shaped charge. It will be dropped off Hayabusa 2; the low gravity leaves the spacecraft enough time to maneuver to the opposite side of the asteroid. A second instrument will then be deployed, the deployable camera (DCAM3). This camera will observe the explosion of the Small Carry-on Impactor instrument. The copper penetrator will strike the asteroid with a velocity of 2 km/s. The crater formed by the impact will be the site of further observations by the spacecraft. The shaped charge will consist of 4.5 kg of plasticized HMX with a 2.5 kg copper liner.
- JAXA Launches Hayabusa 2 Asteroid Probe: NEC conducts manufacturing and testing as probe system coordinator
- Launch of "Hayabusa2" by H-IIA Launch Vehicle No. 26
- Wendy Zukerman (18 August 2010). "Hayabusa 2 will seek the origins of life in space". New Scientist. Retrieved 17 November 2010.
- JAXA Report on Hayabusa-2, May 21st, 2014
- Vilas, Faith (25 February 2008). "SPECTRAL CHARACTERISTICS OF HAYABUSA 2 NEAR-EARTH ASTEROID TARGETS 162173 1999 JU3 AND 2001 QC34". The Astronomical Journal. 135 (4): 1101. Bibcode:2008AJ....135.1101V. doi:10.1088/0004-6256/135/4/1101.
target for the planned Japanese mission Hayabusa 2
- Makoto Yoshikawa (6 January 2011). 小惑星探査ミッション「はやぶさ2」 [Asteroid Exploration Mission "Hayabusa 2"] (PDF). 11th Symposium on Space Science (in Japanese). Retrieved 20 February 2011.
- Clark, Stephen (2014-12-03). "Hayabusa 2 launches on audacious asteroid adventure". spaceflightnow. Retrieved 3 December 2014.
- Japan's next asteroid probe approved for development
- Keiji Tachikawa. The President's New Year Interview, 2007
- Zukerman, Wendy (18 August 2010). "Hayabusa 2 will seek the origins of life in space". New Scientist. Retrieved 17 November 2010.
- "Asteroid probe, rocket get nod from Japanese panel". Spaceflight Now. 11 August 2010. Retrieved 29 October 2012.
- "Japan's next asteroid probe approved for development". Spaceflight Now. 29 January 2012. Retrieved 29 October 2012.
- DLR Asteroid Lander MASCOT
- Graham, William (December 2, 2014). "Japanese H-IIA kicks off Hayabusa 2's asteroid mission". NASASpaceFlight.com. Retrieved 4 December 2014.
- Small Carry-on Impactor (SCI): Its scientific purpose, operation, and observation plan in Hayabysa-2 mission
- Saiki, Takanao; Sawada, Hirotaka; Okamoto, Chisato; Yano, Hajime; Takagi, Yasuhiko; Akahoshi, Yasuhiro; Yoshikawa, Makoto (2013). "Small carry-on impactor of Hayabusa2 mission". Acta Astronautica. 84: 227. Bibcode:2013AcAau..84..227S. doi:10.1016/j.actaastro.2012.11.010.
- Hayabusa 2 Home Page
- JAXA Hayabusa 2 website
- Agency’s Report from ISAS/JAXA
- Hayabusa 2 3D model, Asahi Shinbun
- Technologies for Future Asteroid Exploration: What We Learned From Hyabusa Mission. (PDF, 2006)
- Development of New Sampling Devices for Solar System Small Body Sample Return Program in the Hayabusa Era. (PDF, 2007)