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Please use this identifier to cite or link to this item: http://hdl.handle.net/1853/8031

Title: Impactor Spacecraft Encounter Sequence Design for the Deep Impact Mission
Authors: Kubitschek, Daniel G.
Jet Propulsion Laboratory (U.S.)
Georgia Institute of Technology. Space Systems Design Lab
Subjects : Cometary impacts
Cometary properties
Contingency planning
Deep Impact Comet Encounter
Flyby spacecraft
High rate imaging
Impactor spacecraft
Sequence design
Issue Date: 10-Nov-2005
Publisher: Georgia Institute of Technology
Series/Report no.: SSEC05 Session C;GT-SSEC.C.3
Abstract: On July 4, 2005, another first in space exploration was achieved. NASA’s Deep Impact spacecraft (s/c) released a small, 350 kg Impactor s/c designed to target comet Tempel 1, estimated to be 14 km x 5 km x 5 km in size at the time of release. With a closing speed of approximately 10.3 km/s, the Impactor s/c autonomously guided itself to impact and captured 40 cm resolution images, the highest resolution images ever of the surface of a cometary nucleus, just moments before the collision. The objective of the Impactor s/c was to impact in an illuminated area viewable from the Flyby s/c. This paper describes the Impactor encounter sequence design, execution and contingency planning that contributed to the successful outcome in which all objectives were met.
Description: This conference features the work of authors from: Georgia Tech’s Space Systems Design Lab, Aerospace Systems Design Lab, School of Aerospace Engineering, Georgia Tech Research Institute; NASA’s Jet Propulsion Laboratory, Marshall Space Flight Center, Goddard Space Flight Center, Langley Research Center; and other aerospace industry and academic institutions
Type: Presentation
URI: http://hdl.handle.net/1853/8031
Appears in Collections:SSEC05. Session C: Deep Space Systems
Space Systems Engineering Conference (1st - Atlanta - 2005)

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SSEC_SC3_ppt.pdf586.5 kBAdobe PDFView/Open
SSEC_SC3_doc.pdf553.36 kBAdobe PDFView/Open

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