DocumentCode :
158355
Title :
Replenishing the Mars relay network
Author :
Edwards, C.D. ; Barela, Philip R. ; Gladden, R.E. ; Lee, C.H. ; De Paula, Ramon
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
2014
fDate :
1-8 March 2014
Firstpage :
1
Lastpage :
13
Abstract :
Over the past decade, several NASA Mars orbiters - Mars Global Surveyor, 2001 Mars Odyssey, and the Mars Reconnaissance Orbiter - along with ESA´s Mars Express orbiter, have provided telecommunications relay services to a series of Mars landers, including the Mars Exploration Rovers (Spirit and Opportunity), the Phoenix Lander, and the Mars Science Laboratory´s Curiosity Rover. For each of these missions, relay communications has demonstrated significant benefits, including greatly increased data return from the Martian surface, reduced energy-per-bit cost of communication, and capture of high-rate critical event engineering telemetry during entry, descent, and landing. The orbiters in this relay network, however, are operating well beyond their original design lifetime. To replenish this aging infrastructure, two additional science/relay orbiters are slated for launch in this decade, both equipped with Electra UHF relay transceivers with the plan to provide relay services in addition to each mission´s primary science objectives. On November 18, 2013, NASA successfully launched the Mars Atmosphere and Volatile Evolution Mission (MAVEN). And in January 2016, ESA plans to launch the ExoMars/Trace Gas Orbiter mission, with redundant Electra payloads provided by NASA. Key aspects of each mission relating to its relay service characteristics will be reviewed.
Keywords :
Mars; entry, descent and landing (spacecraft); radio transceivers; radiotelemetry; relay networks (telecommunication); space communication links; space telemetry; telecommunication services; 2001 Mars Odyssey; ESA Mars Express orbiter; Electra UHF relay transceiver; ExoMars-trace gas orbiter mission; MAVEN; Mars Atmosphere and Volatile Evolution Mission; Mars Global Surveyor; Mars Reconnaissance Orbiter; Mars exploration rover; Mars lander; Mars science laboratory curiosity rover; Mars telecommunications relay network service; Martian surface; NASA Mars orbiter; entry descent and landing; high-rate critical event engineering telemetry; mission primary science objective; phoenix lander; redundant electra payload; science-relay orbiter; Mars; NASA; Orbits; Propulsion; Relays; Space vehicles; Transceivers;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2014 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5582-4
Type :
conf
DOI :
10.1109/AERO.2014.6836354
Filename :
6836354
Link To Document :
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