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System Engineering the Space Infrared Interferometric Telescope (SPIRIT)The Space Infrared Interferometric Telescope (SPIRIT) was designed to accomplish three scientific objectives: (1) learn how planetary systems form from protostellar disks and how they acquire their inhomogeneous chemical composition; (2) characterize the family of extrasolar planetary systems by imaging the structure in debris disks to understand how and where planets of different types form; and (3) learn how high-redshift galaxies formed and merged to form the present-day population of galaxies. SPIRIT will accomplish these objectives through infrared observations with a two aperture interferometric instrument. This paper gives an overview of SPIRIT design and operation, and how the three design cycle concept study was completed. The error budget for several key performance values allocates tolerances to all contributing factors, and a performance model of the spacecraft plus instrument system demonstrates meeting those allocations with margin.
Document ID
20070034990
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Hyde, Tristram T.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Leisawitz, David T.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Rinehart, Stephen
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 24, 2013
Publication Date
August 24, 2007
Subject Category
Astrophysics
Meeting Information
Meeting: SPIE International Symposium on Optics and Photonics. UV Optical/IR Space Telescopes: Innovation Technologies and Concepts III
Location: San Diego, CA
Country: United States
Start Date: August 24, 2007
End Date: August 27, 2007
Sponsors: International Society for Optical Engineering
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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