DocumentCode
2906343
Title
Mars Reconnaissance Orbiter: extended dual-purpose mission
Author
Johnston, M. Daniel Dan ; Herman, David E. ; Zurek, Richard W. ; Edwards, Charles D.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
2011
fDate
5-12 March 2011
Firstpage
1
Lastpage
16
Abstract
The Mars Reconnaissance Orbiter (MRO) was launched from Cape Canaveral Air Force Station, Florida, aboard an Atlas V-401 launch vehicle on August 12, 2005 and entered Mars orbit on March 10, 2006. After five months of aerobraking, a series of propulsive maneuvers were used to establish the desired low-altitude science orbit. The spacecraft has been on station in its 255 × 320 km, 3 p.m., primary science orbit since September 2006 performing its scientific and UHF-relay functions. This paper provides a brief status of the prime mission and describes the plans and preparations in work for its recently approved two-year mission extension.
Keywords
Mars; aerospace instrumentation; planetary surfaces; space vehicles; Atlas V-401 launch vehicle; Cape Canaveral Air Force Station; Florida; Mars Reconnaissance Orbiter; UHF-relay functions; aerobraking; extended dual-purpose mission; low-altitude science orbit; propulsive maneuvers; Instruments; Mars; Orbits; Pixel; Reconnaissance; Space vehicles; Spatial resolution;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2011 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-7350-2
Type
conf
DOI
10.1109/AERO.2011.5747277
Filename
5747277
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