Electra (radio)
Electra, more formally called Electra Proximity Payload, is a telecommunications package that acts as a communications relay and navigation aid for Mars spacecraft.[1][2][3] The use of such a relay increases the amount of data that can be returned by two to three orders of magnitude.
The ultimate goal of Electra is to achieve a higher level of system integration, thus allowing significant mass, power, and size reductions, at lower cost, for a broad class of spacecraft.[4]
Overview
The Mars Global Surveyor, Odyssey and Mars Express orbiters carry the first generation of UHF relay payloads. Building on this initial experience, NASA developed a next-generation relay payload, the Electra Proximity Link Payload, which will flew for the first time on the 2005 Mars Reconnaissance Orbiter.[1]
Using Mars orbiters as radio relays to increase data return from rovers and other landers, reduces the mass and power the surface spacecraft need for communications.[5] To build the relay network cost-effectively, NASA includes a relay communications payload on each of its science orbiters. Mars missions launched after 2005 make use of Electra UHF transceiver to provide for any navigation, command, and data-return needs these missions may have. The arriving spacecraft can receive these signals and determine its distance and speed in relation to Mars. This communication allows much more precise navigation.[2]
When NASA's landers and rovers land safely on Mars, Electra can provide precise Doppler data which, when combined with Mars Reconnaissance Orbiter's position information, can accurately determine the location of the lander or rover on the surface of Mars. Electra can also provide UHF coverage to Mars landers and rovers on the surface using its nadir-pointed (pointed straight down at the surface) antenna. This coverage would be important to landed crafts on Mars that might not have sufficient radio power to communicate directly with Earth by themselves.[1]
Key features
- Transceiver that runs the free open source RTEMS operating system.[6]
- Electra's software-defined radio (SDR) provides flexible platform for evolving relay capabilities.[3]
- Fully reprogrammable software/firmware functionality by using field programmable gate array (FPGA) technology.
- CCSDS Proximity-1 Link protocol for interoperable, reliable data transfer.
- Frequency-agile operation across UHF band (390-450 MHz).
- Integrated Doppler navigation and timing services.
- Data rates up to 1 Mbit/s[2]
Deployments
- Mars Reconnaissance Orbiter
- Phoenix
- Mars Exploration Rovers Spirit and Opportunity.
- Mars Science Laboratory entry and descent module.
- Curiosity rover which uses the Electra-lite.
- MAVEN orbiter
- ExoMars Trace Gas Orbiter
References
- ^ a b c "Mars Reconnaissance Orbiter - Electra". NASA. 2005. Retrieved 2013-11-14.
- ^ a b c "NASA's Mars Telecommunications: Evolving to Meet Robotic and Human Mission Needs" (PDF). 8 July 2009. Retrieved 2013-11-14.
- ^ a b Charles D. Edwards, Jr., Thomas C. Jedrey, Eric Schwartzbaum, and Ann S. Devereaux, Ramon DePaula, Mark Dapore, Thomas W. Fischer. "The Electra Proximity Link Payload for Mars Relay Telecommunications and Navigation" (PDF).
{{cite web}}: CS1 maint: multiple names: authors list (link) - ^ Development of the Electra Radio. By Edgar Satorius, Tom Jedrey, David Bell, Ann Devereaux, Todd Ely, Edwin Grigorian, Igor Kuperman, and Alan Lee. 2006. (PDF)
- ^ "NASA". NASA. 17 November 2006. Retrieved 2013-11-14.
- ^ Dale J. Mortensen, Daniel W. Bishop, David Chelmins. "Space Software Defined Radio Characterization to Enable and Reuse" (PDF).
{{cite web}}: CS1 maint: multiple names: authors list (link)
External links
- Development of the Electra Radio. By Edgar Satorius, Tom Jedrey, David Bell, Ann Devereaux, Todd Ely, Edwin Grigorian, Igor Kuperman, and Alan Lee. (PDF)
- Mars Reconnaissance Orbiter Telecommunications - 2006 (PDF)