Hayabusa 2 extension plan: Asteroid selection and trajectory design. (September 2017)
- Record Type:
- Journal Article
- Title:
- Hayabusa 2 extension plan: Asteroid selection and trajectory design. (September 2017)
- Main Title:
- Hayabusa 2 extension plan: Asteroid selection and trajectory design
- Authors:
- Sarli, Bruno Victorino
Tsuda, Yuichi - Abstract:
- Abstract: The Hayabusa 2 mission is targeted to explore the asteroid (162173) 1999 JU 3 and return surface as well as sub-surface samples through a novel impactor. Upon its return, at the end of 2020, the spacecraft will release the capsule for Earth re-entry and drift away from the planet. Based on the current mission profile, the spacecraft is expected to retain 30 kg of xenon propellant for trajectory maneuvers after the capsule is released. This remaining fuel can be used to extend the mission and improve its scientific return by exploring a new target. Work herein outlines an extension plan for Hayabusa 2, detailing the target selection process and its subsequent trajectory design. Due to final Earth escape trajectory, considering the excess velocity and orbital geometry, the only available extension option is an asteroid flyby. One of the most important trajectory characteristic is to maximize the spacecraft's optical detection capabilities. As a result the asteroid 2001 WR 1 is identified as the most promising target candidate. The resulting trajectory uses all the available xenon with 100% duty cycle. Furthermore, the extension lasts for 932 days and offers 1.57 days of optical navigation time for a flyby on June 27, 2023. Highlights: Low-thrust trajectory optimization with optical navigation time objective function. Asteroid 2001 WR1 identified as a possible target for the Hayabusa 2 Extension. Provide trajectory design of the Hayabusa 2 Extension to 4 asteroidAbstract: The Hayabusa 2 mission is targeted to explore the asteroid (162173) 1999 JU 3 and return surface as well as sub-surface samples through a novel impactor. Upon its return, at the end of 2020, the spacecraft will release the capsule for Earth re-entry and drift away from the planet. Based on the current mission profile, the spacecraft is expected to retain 30 kg of xenon propellant for trajectory maneuvers after the capsule is released. This remaining fuel can be used to extend the mission and improve its scientific return by exploring a new target. Work herein outlines an extension plan for Hayabusa 2, detailing the target selection process and its subsequent trajectory design. Due to final Earth escape trajectory, considering the excess velocity and orbital geometry, the only available extension option is an asteroid flyby. One of the most important trajectory characteristic is to maximize the spacecraft's optical detection capabilities. As a result the asteroid 2001 WR 1 is identified as the most promising target candidate. The resulting trajectory uses all the available xenon with 100% duty cycle. Furthermore, the extension lasts for 932 days and offers 1.57 days of optical navigation time for a flyby on June 27, 2023. Highlights: Low-thrust trajectory optimization with optical navigation time objective function. Asteroid 2001 WR1 identified as a possible target for the Hayabusa 2 Extension. Provide trajectory design of the Hayabusa 2 Extension to 4 asteroid candidates. … (more)
- Is Part Of:
- Acta astronautica. Volume 138(2017)
- Journal:
- Acta astronautica
- Issue:
- Volume 138(2017)
- Issue Display:
- Volume 138, Issue 2017 (2017)
- Year:
- 2017
- Volume:
- 138
- Issue:
- 2017
- Issue Sort Value:
- 2017-0138-2017-0000
- Page Start:
- 225
- Page End:
- 232
- Publication Date:
- 2017-09
- Subjects:
- Low-thrust trajectory design -- Asteroid selection -- Hayabusa 2 -- Asteroid flyby
Astronautics -- Periodicals
Outer space -- Exploration -- Periodicals
Astronautics
Periodicals
629.405 - Journal URLs:
- http://www.sciencedirect.com/science/journal/00945765 ↗
http://www.elsevier.com/journals ↗ - DOI:
- 10.1016/j.actaastro.2017.05.016 ↗
- Languages:
- English
- ISSNs:
- 0094-5765
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library DSC - 0596.750000
British Library DSC - BLDSS-3PM
British Library HMNTS - ELD Digital store - Ingest File:
- 12817.xml