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Launch Window Trade Analysis for the James Webb Space Telescope The James Webb Space Telescope (JWST) is a large-scale space telescope mission designed to study fundamental astrophysical questions ranging from the formation of the universe to the origin of planetary systems and the origins of life. JWSTs orbit design is a Libration Point Orbit (LPO) around the Sun-Earth/Moon (SEM) L2 point for a planned mission lifetime of 10.5 years. The launch readiness period for JWST is from Oct 1st, 2018 November 30th, 2018. This paper presents the first launch window analysis for the JWST observatory using finite-burn modeling; previous analysis assumed a single impulsive midcourse correction to achieve the mission orbit. The physical limitations of the JWST hardware stemming primarily from propulsion, communication and thermal requirements alongside updated mission design requirements result in significant launch window within the launch readiness period. Future plans are also discussed.
Document ID
20160001318
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Yu, Wayne H.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Richon, Karen
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
February 1, 2016
Publication Date
May 5, 2014
Subject Category
Astrodynamics
Report/Patent Number
GSFC-E-DAA-TN14126
Meeting Information
Meeting: International Symposium on Space Flight Dynamics
Location: Laurel, MD
Country: United States
Start Date: May 5, 2014
End Date: May 9, 2014
Sponsors: Johns Hopkins Univ.
Funding Number(s)
OTHER: 595
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
window
James Webb Space Telescope
launch
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