This article is about 2014 mission.
For cancelled mission, see
Hayabusa Mk2.
Hayabusa 2
|
|
Mission type |
Asteroid sample return |
---|
Operator |
JAXA |
---|
COSPAR ID |
2014-076A |
---|
SATCAT № |
40319 |
---|
Website |
Hayabusa 2 on jaxa.jp |
---|
|
Spacecraft properties |
---|
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 (2014-12-03UTC04:22Z)[1] |
---|
Rocket |
H-IIA 202 |
---|
Launch site |
LA-Y, Tanegashima Space Center |
---|
|
End of mission |
---|
Landing date |
December 2020 (planned) |
---|
|
Flyby of Earth |
---|
Closest approach |
December 2015 |
(162173) 1999 JU3 orbiter |
---|
Orbital insertion |
June 2018 (planned) |
---|
Departed orbit |
December 2019 (planned) |
---|
|
Hayabusa 2 is an asteroid sample return mission operated by the Japanese space agency, JAXA. It follows on from Hayabusa and addresses weak points learned from that mission.[2]
Mission overview
Initially, launch was planned for 30 November 2014 (13:23 local time),[3][4][5] but was delayed to 3 December 2014 04:22 UTC (4 December 2014 13:22:04 local time).[6]
The target is asteroid (162173) 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.[5]
The spacecraft features ion engines, upgraded guidance and navigation technology, antennas and attitude control systems.[7] Operations at the asteroid will be similar to those of the previous Hayabusa, but with an explosive device to dig the asteroid surface for fresh sample material.[5]
Funding and international cooperation
Hayabusa 2 was agreed by the Space Activities Commission, a board governing funding for the Japanese space program, during 2006 and was announced in a new year interview with JAXA president Keji Tachikawa.[8]
In July 2009, at the 27th ISTS (International Symposium on Space Technology and Science) conference in Japan, presentations were given that elaborated upon the most recent Hayabusa 2 mission concept. Makoto Yoshikawa of JAXA presented a paper entitled "Hayabusa Follow-on Asteroid Sample Return Missions." Dr. Yoshikawa stated that JAXA has a new proposal for Hayabusa 2, namely that the mission have two spacecraft with one specifically being an impactor.
In August 2010, JAXA got the go-ahead from the Japanese government to begin development of Hayabusa 2. The estimated cost of the project is 16.4 billion yen.[9][10]
NEC Corp. of Tokyo announced in January 2012 that it was beginning system design of the 590 kg (1,300-pound) spacecraft, its Ka-band communications system and an intermediate infrared camera. NEC was the builder of the Hayabusa probe.[11]
Instruments
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.[12] 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.[13]
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.[13] 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 explosion will form a copper penetrator hitting the asteroid with a velocity of 2 km/s. The crater created by the impact will be the site of further observations by the onboard instruments.[14] The shaped charge will consist of 4.5 kg of plasticized HMX and a 2.5 kg copper liner.[15]
References
- ↑ 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
- ↑ 5.0 5.1 5.2 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
- ↑ 13.0 13.1 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.
See also
External links
Japanese space program |
---|
| Organizations | |
---|
| Earth observation | Completed | |
---|
| In operation | |
---|
| Planned | |
---|
|
---|
| Communications, broadcasting and positioning | Completed |
- Sakura (1
- 2a
- 2b
- 3a
- 3b)
- Yuri
- BS
- Kakehashi
- N-STAR
- Kirari
- MBSat
|
---|
| In operation | |
---|
| Planned | |
---|
|
---|
| Engineering tests | Completed | |
---|
| In operation | |
---|
| Planned |
- PETSAT
- SERVIS-3
- SLATS
- DESTINY
|
---|
| Cancelled | |
---|
|
---|
| Private miniaturized satellites | Completed | |
---|
| In operation |
- Fuji-3
- CUTE
- XI
- SEEDS
- Raijin
- Kiseki
- Hitomi
- Horyu
- PROITERES
- RAIKO
- FITSAT-1
|
---|
| Planned |
- WNI satellite
- SPROUT
- TSUBAME
- QSAT-EOS
- SOMESAT
|
---|
|
---|
| Astronomical observation | Completed | |
---|
| In operation | |
---|
| Planned | |
---|
| Cancelled | |
---|
|
---|
| Lunar and planetary exploration | Completed | |
---|
| In operation | |
---|
| Failed | |
---|
| Planned | |
---|
| Cancelled | |
---|
|
---|
| Reconnaissance | Completed | |
---|
| In operation | |
---|
| Planned | |
---|
|
---|
| Human spaceflight | Completed | |
---|
| In operation | |
---|
| Planned | |
---|
| Cancelled | |
---|
|
---|
|
- Italics indicates projects in development.
- Superscripts indicate joint development with1NASA, 2ESA, 3ASI, 4CSA, 5RKA, 6AEB and 7INPE.
|
|
|
---|
| Orbiters | | |
---|
| Landers | |
---|
| Flybys | |
---|
| Planned | |
---|
| Proposed | |
---|
| Cancelled | |
---|
|
- Italics indicate active missions.
|
|
Planetary defense |
---|
| Main topics | | |
---|
| Defense | |
---|
| Space probes | |
---|
| NEO tracking | |
---|
| Organizations | |
---|
| Potential threats | |
---|
| Films/video | |
---|
|
|
---|
| | | Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |
|