Cassini spacecraft design

Roger Gibbs

doi:10.1117/12.253425

7 October 1996 Cassini spacecraft design

Roger Gibbs

Proceedings Volume 2803, Cassini/Huygens: A Mission to the Saturnian Systems; (1996) https://doi.org/10.1117/12.253425
Event: SPIE's 1996 International Symposium on Optical Science, Engineering, and Instrumentation, 1996, Denver, CO, United States

Abstract

The Cassini spacecraft will explore the planet Saturn and its rings and moons with an orbiter and atmospheric entry probe, both of which have a sophisticated set of science instruments. The spacecraft design is responsive to mission and science objectives, and is influenced by technical and programmatic constraints e.g., a cost cap, fixed schedule, space environment, and interfaces to other fixed systems like the launch vehicle and ground system. The spacecraft design must also consider the limited post-launch resources allocated to do the flight operations. This paper presents an overview of the spacecraft system design with emphasis given to the orbiter and only a high level summary of the probe.

Citation Download Citation

Roger Gibbs "Cassini spacecraft design", Proc. SPIE 2803, Cassini/Huygens: A Mission to the Saturnian Systems, (7 October 1996); https://doi.org/10.1117/12.253425

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