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Proceedings Paper

Spitzer Space Telescope mission design
Author(s): Johnny H. Kwok; Mark D. Garcia; Eugene Bonfiglio; Stacia M. Long
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Paper Abstract

This paper gives a description of the mission design, launch, orbit, and navigation results for the Spitzer space telescope mission. The Spitzer telescope was launched by the Delta II Heavy launch vehicle into a heliocentric Earth trailing orbit. This orbit is flown for the first time and will be used by several future astronomical missions such as Kepler, SIM, and LISA. This paper describes the launch strategy for a winter versus a summer launch and how it affects communications. It also describes how the solar orbit affects the design and operations of the Observatory. It describes the actual launch timeline, launch vehicle flight performance, and the long term behavior of the as flown orbit. It also provides the orbit knowledge from in-flight navigation data.

Paper Details

Date Published: 12 October 2004
PDF: 10 pages
Proc. SPIE 5487, Optical, Infrared, and Millimeter Space Telescopes, (12 October 2004); doi: 10.1117/12.551598
Show Author Affiliations
Johnny H. Kwok, Jet Propulsion Lab. (United States)
Mark D. Garcia, Jet Propulsion Lab. (United States)
Eugene Bonfiglio, Jet Propulsion Lab. (United States)
Stacia M. Long, Jet Propulsion Lab. (United States)

Published in SPIE Proceedings Vol. 5487:
Optical, Infrared, and Millimeter Space Telescopes
John C. Mather, Editor(s)

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