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# | #dysonswarm uses SI units and Earth time (day,hour,year,kg,s,mol,cd,Ampere,Kelvin,m). [https://en.wikipedia.org/wiki/Scientific_notation#E-notation E-notation] with no spaces is acceptable. | ||
#The host planet [https://en.wikipedia.org/wiki/Mercury_(planet) Mercury] ("Host") is low-gravity which will help get the swarm into orbit. It is close to the the swarm | #The host planet [https://en.wikipedia.org/wiki/Mercury_(planet) Mercury] ("Host") is low-gravity which will help get the swarm into orbit. It is close to the the swarm which orbits between the host and the sun. | ||
#[https://en.wikipedia.org/wiki/Avogadro_constant Avogadro] says there are 6E23 atoms in every mol of material. A mol of the elements of the host is 54g. | #[https://en.wikipedia.org/wiki/Avogadro_constant Avogadro] says there are 6E23 atoms in every mol of material. A mol of the elements of the host is 54g. | ||
#The raw material for the swarm and its factories is [https://www.lenntech.com/periodic/mass/atomic-mass.htm elements]. These elements will be extracted from the host. There are fewer then a hundred elements needed. | #The raw material for the swarm and its factories is [https://www.lenntech.com/periodic/mass/atomic-mass.htm elements]. These elements will be extracted from the host. There are fewer then a hundred elements needed. | ||
#The construction material for the swarm and its factories is the [https://en.wikipedia.org/wiki/Microbotics | #The construction material for the swarm and its factories is the [https://en.wikipedia.org/wiki/Microbotics minibot]. This is a general purpose machine possibly consisting of fewer than 1E20 atoms (0.25g). Teams will specify the performance requirements and design of the minibots. | ||
#The 1% of the host which is available as raw material has a mass of 3.3E21kg and makes | #The 1% of the host which is available as raw material has a mass of 3.3E21kg and makes at least 1.3E25 minibots with 0.1% refinery efficiency. | ||
#There may be four generations of mirrors... | #There may be four generations of mirrors... | ||
#*The fab has to arrive on site with a prefabricated energy generating capacity which may involve taking first-gen mirrors, or maybe just solar panels. | #*The fab has to arrive on site with a prefabricated energy generating capacity which may involve taking first-gen mirrors, or maybe just solar panels. | ||
#*Second-gen ground-based mirrors and planet-orbit railgun are ground-manufactured to ramp up energy. | #*Second-gen ground-based mirrors and planet-orbit railgun are ground-manufactured to ramp up energy. | ||
#*Third-gen mirrors are launched as 1-mirror factory packs and made in zero-G to swarm in Mercury orbit, powering just the site which makes the escape-velocity railgun. | #*Third-gen mirrors are launched as 1-mirror factory packs and made in zero-G to swarm in Mercury orbit, powering just the site which makes the escape-velocity railgun. | ||
#*Fourth-gen mirrors are launched as 1-mirror factory packs and made in zero-G to swarm in Solar orbit, powering the whole system. We have a likely mass limit of 20 tonnes on each launch based on a 1km{{sq}} mirror at 5g/m{{sq}} = 5 tonnes and a feasible overhead of 3x for the factory which makes the mirror in zero-G and the coupled power transmitter. Is there an efficiency benefit in orders-of-magnitude larger mirrors or do we leave that choice to the swarm which will replace this prototype? | #*Fourth-gen mirrors,if the solar swarm differs in design to those in Mercury orbit, are launched as 1-mirror factory packs and made in zero-G to swarm in Solar orbit, powering the whole system. We have a likely mass limit of 20 tonnes on each launch based on a 1km{{sq}} mirror at 5g/m{{sq}} = 5 tonnes and a feasible overhead of 3x for the factory which makes the mirror in zero-G and the coupled power transmitter. Is there an efficiency benefit in orders-of-magnitude larger mirrors or do we leave that choice to the swarm which will replace this prototype? | ||
#The site needs receivers to translate light to usable power. Forms of distribution around the site could include microwave/WiFi, light, electric, hydraulic. Some components also definitely need a power store - any form of railgun, for example. | #The site needs receivers to translate light to usable power. Forms of distribution around the site could include microwave/WiFi, light, electric, hydraulic. Some components also definitely need a power store - any form of railgun, for example. | ||
#An initial estimate of [[cost]] has been made and requires continuous improvement as resolution of the problems brings matters into a finer focus. | |||
Latest revision as of 13:29, 3 October 2020
- dysonswarm uses SI units and Earth time (day,hour,year,kg,s,mol,cd,Ampere,Kelvin,m). E-notation with no spaces is acceptable.
- The host planet Mercury ("Host") is low-gravity which will help get the swarm into orbit. It is close to the the swarm which orbits between the host and the sun.
- Avogadro says there are 6E23 atoms in every mol of material. A mol of the elements of the host is 54g.
- The raw material for the swarm and its factories is elements. These elements will be extracted from the host. There are fewer then a hundred elements needed.
- The construction material for the swarm and its factories is the minibot. This is a general purpose machine possibly consisting of fewer than 1E20 atoms (0.25g). Teams will specify the performance requirements and design of the minibots.
- The 1% of the host which is available as raw material has a mass of 3.3E21kg and makes at least 1.3E25 minibots with 0.1% refinery efficiency.
- There may be four generations of mirrors...
- The fab has to arrive on site with a prefabricated energy generating capacity which may involve taking first-gen mirrors, or maybe just solar panels.
- Second-gen ground-based mirrors and planet-orbit railgun are ground-manufactured to ramp up energy.
- Third-gen mirrors are launched as 1-mirror factory packs and made in zero-G to swarm in Mercury orbit, powering just the site which makes the escape-velocity railgun.
- Fourth-gen mirrors,if the solar swarm differs in design to those in Mercury orbit, are launched as 1-mirror factory packs and made in zero-G to swarm in Solar orbit, powering the whole system. We have a likely mass limit of 20 tonnes on each launch based on a 1km2 mirror at 5g/m2 = 5 tonnes and a feasible overhead of 3x for the factory which makes the mirror in zero-G and the coupled power transmitter. Is there an efficiency benefit in orders-of-magnitude larger mirrors or do we leave that choice to the swarm which will replace this prototype?
- The site needs receivers to translate light to usable power. Forms of distribution around the site could include microwave/WiFi, light, electric, hydraulic. Some components also definitely need a power store - any form of railgun, for example.
- An initial estimate of cost has been made and requires continuous improvement as resolution of the problems brings matters into a finer focus.