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ARTEMIS Mission Overview: From Concept to OperationsARTEMIS (Acceleration, Reconnection, Turbulence and Electrodynamics of the Moon's Interaction with the Sun) repurposed two spacecraft to extend their useful science (Angelopoulos, 2010) by moving them via lunar gravity assists from elliptical Earth orbits to L1 and L2 Earth-Moon libration orbits and then to lunar orbits by exploiting the Earth-Moon-Sun dynamical environment. This paper describes the complete design from conceptual plans using weak stability transfer options and lunar gravity assist to the implementation and operational support of the Earth-Moon libration and lunar orbits. The two spacecraft of the ARTEMIS mission will have just entered lunar orbit at this paper's presentation.
Document ID
20180001143
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Folta, David
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Sweetser, Theodore
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
February 13, 2018
Publication Date
July 31, 2011
Subject Category
Lunar And Planetary Science And Exploration
Spacecraft Design, Testing And Performance
Astrodynamics
Report/Patent Number
LEGNEW-OLDGSFC-GSFC-LN-1220
AAS 11-510
Report Number: LEGNEW-OLDGSFC-GSFC-LN-1220
Report Number: AAS 11-510
Meeting Information
Meeting: American Astronautical Society/American Institute of Aeronautics and Astronautics (AAS/AIAA) Astrodynamics Specialist Conference
Location: Girdwood, AK
Country: United States
Start Date: July 31, 2011
End Date: August 4, 2011
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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