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The Effects of Propellant Slosh Dynamics on the Solar Dynamics ObservatoryThe Solar Dynamics Observatory (SOO) mission, which is part of the Living With a Star program, was successfully launched and deployed from its Atlas V launch vehicle on February 11, 2010. SOO is an Explorer-class mission now operating in a geosynchronous orbit (GEO). The basic mission is to observe the Sun for a very high percentage of the 5-year mission (10-year goal) with long stretches of uninterrupted observations and with constant, high-data-rate transmission to a dedicated ground station located in White Sands, New Mexico. Almost half of SDO's launch mass was propellant, contained in two large tanks. To ensure performance with this amount of propellant, a slosh analysis was performed prior to launch. This paper provides an overview of the SDO slosh analysis, the on-orbit experience, and the lessons learned.
Document ID
20180001146
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Mason, Paul
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Starin, Scott R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
February 13, 2018
Publication Date
July 25, 2011
Subject Category
Propellants And Fuels
Fluid Mechanics And Thermodynamics
Solar Physics
Report/Patent Number
LEGNEW-OLDGSFC-GSFC-LN-1212
Meeting Information
Meeting: O''Reilly Open Source Convention
Location: Portland, OR
Country: United States
Start Date: July 25, 2011
End Date: July 29, 2011
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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