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Landsat Data Continuity Mission (LDCM) Ascent and Operational Orbit DesignFor the past 40-years, Landsat Satellites have collected Earth's continental data and enabled scientists to assess change in the Earth's landscape. The Landsat Data Continuity Mission (LDCM) is the next generation satellite supporting the Landsat science program. LDCM will fly a 16-day ground repeat cycle, Sun-synchronous, frozen orbit with a mean local time of the descending node ranging between 10:10 am and 10:15 am. This paper presents the preliminary ascent trajectory design from the injection orbit to its final operational orbit. The initial four burn ascent design is shown to satisfy all the LDCM mission goals and requirement and to allow for adequate flexibility in re-planning the ascent.
Document ID
20120009335
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Mann, Laurie M.
(AI Solutions, Inc. Lanham, MD, United States)
Nicholson, Ann M.
(AI Solutions, Inc. Lanham, MD, United States)
Good, Susan M.
(AI Solutions, Inc. Lanham, MD, United States)
Woodard, Mark A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 25, 2013
Publication Date
January 29, 2012
Subject Category
Astrodynamics
Report/Patent Number
Preprint AAS 12-254
GSFC.CP.6034.2012
Report Number: Preprint AAS 12-254
Report Number: GSFC.CP.6034.2012
Meeting Information
Meeting: 22nd AAS/AIAA Space Flight Mechanics Meeting
Location: Charleston, SC
Country: United States
Start Date: January 29, 2012
End Date: February 2, 2012
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronomical Society
Funding Number(s)
CONTRACT_GRANT: NNG10CP02C
Distribution Limits
Public
Copyright
Public Use Permitted.
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