User:Jrmyismvp/Electra Proximity Payload

Electra Proximity Payload,or Electra for short, is a software-defined radio (first used on the Mars Reconnaissance Orbiter, launched on August 12, 2005) which is used as a communications relay and navigation aid for space crafts. Generally a space craft works together with an orbiter equipped with an Ultra high frequency (UHF) Electra radio, which can then relay the signal from the spacecraft to Earth, as well as navigation commands from Earth to the spacecraft through the orbiter. Electra has been used for many of the Mars exploration missions. The Electra radio plays an important role in obtaining new information or discoveries found by a spacecraft and then allowing this information to be delivered to Earth. There are possible plans of the Electra radio being used for future Mars missions.

Features

Electra is NASA's first highly capable software defined radio for space missions. The Electra radio is described as elegant with a compact design based around a reprogrammable radiation-tolerant field programmable gate array (FPGA). What makes it unique as a software defined radio is its flexibility to operate and be reconfigured to different frequencies. Older radios could only operate under a certain frequency and all other equipment was limited to that one frequency in order to be compatible. The Electra radio can be reprogrammed to be able to upgrade and make adjustment according to whatever needs or complications that may arise in the future, such as operating at higher or lower power while taking into account the energy consumption.

Uses

Electra is currently NASA's standard tested radio, most commonly used on NASA's Mars Exploration Missions. The Electra radio is used on the Mars rovers Spirit, Opportunity, and the most recent success Curiosity. All these rovers work with the UHF Electra radio on the Mars Reconnaissance Orbiter which then relays information back and forth between the rovers and Earth. Information from new discoveries made by the rovers on the Martian surface is sent to Earth using the Electra radio. The transfer of information and commands with the rovers is monitored by JPL.

Technical Specifications

C/TT-510 Electra-Lite Transceiver

Data Rates:

• Tx (1, 6, 12 Mbps)
• Rx (up to 10 Mbps)
• Relay (1,2,4,8,16,32,64,128,256,1024,2048,4096 ksps)

General:

• Modulation Balance: Amp.<0.25 dB;Phase <+/- 2°
• Implementation Loss: Within 2 dB of theory

Power Requirements:

• Input Voltage: +22 to +36 Vdc
• Input Power: 65W FD (typ); 15W Standby
• 12.6W Boot Safe (typ)

Radiation:

• Total Dose: 20 Krad 100 mil Al

Environmental Specifications:

• Temperature: -50°C to +110°C (non-operating)/-45°C to +72°C (operating)
• Vibration: Random; 7.9 grms, 3-axis
• Shock: 2000 g

Physical:

• Footprint: 6.35” (W) x 8” (D) x 4.11” (H)
• Weight: 3 kg / 6.61 lbs (typ)

Future

It has been proposed that a Mars rover mission, the Mars Astrobiology Explorer-Chacher mission (MAX-C) would be launched in May 2018 by NASA. MAX-C would carry the European Space Agency’s (ESA’s) ExoMars rover (EXM) and the NASA Mid-Range rover (MAX-C rover). They would arrive on the Martian surface in January 2019. Both the rovers would operate along with an orbiter proposed to launch in 2016 in which all space crafts would be equipped with an Electra payload. Further work needs to be done on techniques to communicate with both rovers simultaneously. As we venture farther out into deep space, the Electra radio will not be as effective and so it will not be used on such missions, but for now while our primary focus is on Mars, the Electra radio will still be used for these missions.

External links

• example.com