Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
isotope
|
| gptkbp:coolingSystem |
passive cooling
|
| gptkbp:designedFor |
gptkb:NASA
lunar missions planetary missions deep space missions |
| gptkbp:developedBy |
gptkb:U.S._Department_of_Energy
|
| gptkbp:fuelType |
plutonium-238 dioxide
|
| gptkbp:fullName |
gptkb:Multi-Mission_Radioisotope_Thermoelectric_Generator
|
| https://www.w3.org/2000/01/rdf-schema#label |
MMRTG
|
| gptkbp:introducedIn |
2011
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin_Space_Systems
gptkb:Teledyne_Energy_Systems |
| gptkbp:operationalLifetime |
at least 14 years
|
| gptkbp:powerOutput |
approximately 110 watts
|
| gptkbp:purpose |
provide electrical power and heat for spacecraft
|
| gptkbp:reliability |
high
|
| gptkbp:technology |
thermoelectric generator
|
| gptkbp:usedOn |
gptkb:Curiosity_rover
gptkb:Mars_Science_Laboratory gptkb:Perseverance_rover |
| gptkbp:weight |
approximately 45 kg
|
| gptkbp:bfsParent |
gptkb:Mars_2020_Perseverance_Rover
gptkb:Perseverance_Rover gptkb:Perseverance_rover |
| gptkbp:bfsLayer |
5
|