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Dynamic Orbital Slingshot for Rendezvous with Interstellar Objects

Completed TRL 2 (started at 1, targeting 2)

Description

The study of asteroids and comets has revealed a treasure trove of information about the formation and history of our solar system. In 2017, the first InterStellar Object (ISO) Oumuamua was discovered and recently, in August 2019 a second object was discovered. The second object will fly by the Sun in December 2019. The existence of these ISOs offers us a great scientific opportunity to develop a detailed understanding of the formation and history of other star systems. In this proposal, a Dynamic Orbital Slingshot concept is proposed for a rapid flyby and rendezvous mission to an ISO (e.g., Interstellar asteroids, comets). Studying ISOs up close will be critical to answering fundamental scientific questions, however, due to their high heliocentric velocities and relatively short lead time, this may be extremely difficult with current satellite propulsion systems. This work proposes the use of a statite, an artificial satellite that employs a solar sail to continuously modify its orbit allowing it to hover in place. The proposed system has the smallest possible orbital period for a given distance. In essence, the solar sail is stationary in the heliocentric frame and once an ISO is detected the system can deliver a CubeSat on either a flyby trajectory or on a rendezvous trajectory (with propulsion). The proposed use of statites for fast response to newly detected ISO is at the center of the innovation for the proposed work and this study will investigate the feasibility of rapid flyby and rendezvous mission.

Benefits

The existence of ISOs offer us a great scientific opportunity to develop a detailed understanding of the formation and history of other star systems. However, due to their high heliocentric velocities and relatively short lead time, this may be extremely difficult with current satellite propulsion systems. The proposed approach can respond to a newly detected ISO within 2-3 month to perform a flyby. The proposed approach also allows for rapid response rendezvous missions.

Details

Technology areaGN&C > Navigation Technologies > Rendezvous, Proximity Operations, and Capture Trajectory Design and Orbit Determination
ProgramNASA Innovative Advanced Concepts (NIAC)
Lead organizationMassachusetts Institute of Technology, Cambridge, MA
Start date2020-05-27
End date2021-03-12

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