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by ProblemFactory
3028 days ago
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> The missions targeted by this technology are GOCE-like spacecrafts which by design must fly low Once the technology matures, it could be used by more missions. Flying low has its benefits: * Lower latency for communication satellites, * Better resolution for Earth imaging / spy satellites, * When the satellite fails, it quickly deorbits by itself. Until now, flying low has just not been economical, but if this thruster has similar lifetime to medium and high orbit satellites, then many more missions could choose lower orbits. |
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This also means that failure recovery will be quite tricky if possible at all. There are some downsides to other points too: such a satellite would work at very thin margins due to the thruster being inefficient with air as a propellant. Its ground swath width will be lower, coverage will be worse, requiring more ground stations (remote sensing is very often limited by the downlink bandwidth). Also, some kind of aerodynamic shape will be required, limiting its capabilities and power budget. (electric propulsion needs a lot of power itself)