Electra, formally called the Electra Proximity Link Payload, is a telecommunications package that acts as a communications relay and navigation aid for Mars spacecraft and rovers. 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.
The Mars Global Surveyor, Mars 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 flew for the first time on the 2005 Mars Reconnaissance Orbiter.
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. A special feature is that it can actively adjust the data rate during a communication session – slower when the orbiter is near the horizon from the surface robot's perspective, faster when it is overhead. 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.
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.
- Transceiver that runs the free open source RTEMS operating system.
- Electra's software-defined radio (SDR) provides flexible platform for evolving relay capabilities.
- Fully reprogrammable software/firmware functionality by using field-programmable gate array (FPGA) technology.
- CCSDS Proximity-1 Space 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:8
- Mars Reconnaissance Orbiter (2nd generation UHF, the Electra Proximity Link Payload)
- Mars Science Laboratory entry and descent module
- Curiosity rover which uses the Electra-lite
- MAVEN orbiter
- ExoMars Trace Gas Orbiter, two Electra radios
- Future deployments
- Mars Global Surveyor (1st generation UHF relay payload)
- 2001 Mars Odyssey(1st generation UHF relay payload)
- Mars Express (1st generation UHF relay payload)
- "MRO Spacecraft and Instruments: Electra". NASA. 22 November 2007. Retrieved 14 November 2013.
- Schier, Jim; Edwards, Chad (8 July 2009). "NASA's Mars Telecommunications: Evolving to Meet Robotic and Human Mission Needs" (PDF). NASA. Retrieved 14 November 2013.
- Edwards, Jr., Charles D.; Jedrey, Thomas C.; Schwartzbaum, Eric; Devereaux, Ann S.; DePaula, Ramon; Dapore, Mark (2003). The Electra Proximity Link Payload for Mars Relay Telecommunications and Navigation. 54th International Astronautical Congress. 29 September-3 October 2003. Bremen, German. doi:10.2514/6.IAC-03-Q.3.a.06.
- Satorius, Edgar; Jedrey, Tom; Bell, David; Devereaux, Ann; Ely, Todd; et al. (2006). "The Electra Radio" (PDF). In Hamkins, Jon; Simon, Marvin K. (eds.). Autonomous Software-Defined Radio Receivers for Deep Space Applications. Deep Space Communications and Navigation Series. NASA/Jet Propulsion Laboratory. Archived from the original (PDF) on 3 October 2006.
- Webster, Guy (17 November 2006). "NASA's Newest Mars Orbiter Passes Communications Relay Test". NASA. Retrieved 14 November 2013.
- "NASA Electra Radio for the Trace Gas Orbiter". European Space Agency. 2 July 2014.
- Mortensen, Dale J.; Bishop, Daniel W.; Chelmins, David T. (2012). Space Software Defined Radio Characterization to Enable Reuse (PDF). 30th AIAA International Communications Satellite Systems Conference. 24–27 September 2012. Ottawa, Canada. doi:10.2514/6.2012-15124.
- Webster, Guy (2 July 2014). "NASA Radio Delivered for Europe's 2016 Mars Orbiter". NASA/JPL. Retrieved 22 April 2018.
- Ormston, Thomas (18 October 2016). "Listening to an Alien Landing". European Space agency.
- Novak, Keith S.; Kempenaar, Jason G.; Redmond, Matthew; Bhandari, Pradeep (2015). Preliminary Surface Thermal Design of the Mars 2020 Rover (PDF). 45th International Conference on Environmental Systems. 12–16 July 2015. Bellevue, Washington.
- Taylor, Jim; Lee, Dennis K.; Shambayati, Shervin (September 2006). Mars Reconnaissance Orbiter Telecommunications (PDF). DESCANSO Design and Performance Summary Series. NASA/Jet Propulsions Laboratory.
- Webster, Guy; Neal-Jones, Nancy (28 February 2014). "Relay Radio on Mars-Bound NASA Craft Passes Checkout". NASA.
- "Newest NASA Mars Orbiter Demonstrates Relay Prowess". University of Colorado Boulder. 10 November 2014.