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
Link To Document :
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