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Return to the moon - The Lunar Observer missionThe Lunar Observer mission seeks to understand the moon in its global context. Motivation for this project comes from scientific interest and the need for robotic precursor missions in the proposed Space Exploration Initiative. The multiple roles to be performed by this mission mean that the trajectory design process promises to be quite complex and unique. The choice of launch vehicle, launch opportunity and daily launch window are affected by the selection of the translunar transfer trajectory, as well as the arrival conditions desired at lunar orbit insertion. The length of the mission and the tight lunar orbit control requirements determine the design of the circumlunar portions of the Lunar Observer mission.
Document ID
19900065926
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cook, Richard A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sergeyevsky, Andrey B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Belbruno, Edward A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sweetser, Theodore H.
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Astronautics (General)
Report/Patent Number
AIAA PAPER 90-2888
Report Number: AIAA PAPER 90-2888
Meeting Information
Meeting: AIAA/AAS Astrodynamics Conference
Location: Portland, OR
Country: United States
Start Date: August 20, 1990
End Date: August 22, 1990
Accession Number
90A52981
Distribution Limits
Public
Copyright
Other

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