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Diving Deeper: Exploring the Feasibility of Lowering Cassini’s Final OrbitsDuring the final five orbits of Cassini’s mission, the spacecraft will get closer to Saturn than it has ever been. These five orbits were designed to be as deep in the atmosphere as Cassini could safely fly; however, recent occultation data of Saturn’s atmosphere suggest that it is contracting. Given this contraction, the primary concern during these orbits has shifted from spacecraft health and safety to loss of science value. This paper explores a scenario for modifying the Cassini spacecraft’s trajectory, during these final orbits, such that it dips deeper into Saturn’s atmosphere. This scenario describes the method for in-situ detection of Saturn’s atmospheric state, the locations and sizes of maneuvers that would reduce the final periapsis altitudes, the effects of such maneuvers on the remaining trajectory, and the risks involved. The result is that a periapsis-lowering, “pop-down” maneuver is feasible during Cassini’s final orbits. Risk to the spacecraft is minimized by using the attitude control thrusters as density detectors during the first three atmospheric transits of the final five orbits. Should these transits reveal sufficiently low density and should sufficient propellant remain, then the Cassini project will consider performing the maneuver.
Document ID
20190028473
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Sturm, Erick J., II
(Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Date Acquired
August 1, 2019
Publication Date
March 4, 2017
Subject Category
Astrodynamics
Report/Patent Number
JPL-CL-CL#17-5349
Report Number: JPL-CL-CL#17-5349
Meeting Information
Meeting: 2017 IEEE Aerospace Conference
Location: Big Ski, MT
Country: United States
Start Date: March 4, 2017
End Date: March 11, 2017
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Other

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