Asteroid 99942, also known as Apophis, will make a close approach to Earth on April 13, 2029, coming within 31,860 kilometers of Earth (within the geostationary belt), presenting a unique opportunity to study its characteristics and trajectory, enhancing our understanding of near-Earth objects and planetary defense.
The symposium will focus primarily on evaluating the expected science return from a rendezvous mission to Apophis during its close Earth flyby that is being developed jointly by Caltech, JPL and CNES, along with industry partners. The science motivation for the mission focuses on what can be learned regarding the strength and interior structure of Apophis from observations before and after its closest approach, as well as an active bistatic radar experiment. The adequacy of the planned instruments and operational plan, and the feed forward into designing and modeling the deflection of a hazardous asteroid will be assessed. Suggestions for additional measurements that would enhance the science return will be considered. The objectives of this KISS symposium are to:
- Review what we can learn from specific measurements at Apophis and how they will advance the science of planetary defense, using the Small Bodies Assessment Group’s Apophis Specific Action Team Report as a backdrop
- Provide guidance to the Apophis mission planning team at Caltech and JPL, to ensure the highest science return within cost and other constraints
- Define how the open data will be utilized to apply knowledge gained regarding the nature of rubble pile asteroids in general, and Apophis in particular to reduce modeling uncertainties in designing a future deflection attempt
Key outcomes of our Symposium will be:
- A set of recommendations to the mission team regarding the highest priority instrument capabilities and data products to exploit the Apophis close flyby opportunity and improve readiness for mitigating a hazardous asteroid
- A plan for follow-on activities to prepare for using the mission data to understand Apophis’ interior and provide inputs to asteroid deflection modeling codes