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The impossible task of traveling 25.6 trillion miles to Alpha Centauri, our closest star, is now possible. Using a Directed Energy System for Targeting of Asteroids and exploRation (DE-STAR), a versatile, scalable phased-array laser system, it can be reached in a short 16 years. Our project entails carrying out both computational and experimental studies of specific uses of DE-STAR to investigate photon recycling and spacecraft propulsion. Photon recycling is a unique term used to describe a form of energy conservation relative to this project. This effect will greatly improve the efficiency of spacecraft making interstellar flight more plausible. What lies beyond our solar system is one of the biggest mysteries of mankind and it finally has the potential to be solved.
Wafer Scale Spacecraft. Recent work at UCSB on Si photonics now allows us to design and build a "spacecraft on a wafer". The recent (UCSB) work in phased array lasers on a wafer for ground-based optical communications combined with the ability to combine optical arrays (CMOS imagers for example) and MEMS accelerometers and gyros as well as many other sensors and computational abilities allows for extremely complex and novel systems. Traditional spacecraft are still largely built so that the mass is dominated by the packaging and interconnects rather than the fundamental limits on sensors. Our approach is similar to comparing a laptop of today to a super computer with similar power of 20 years ago and even a laptop is dominated by the human interface (screen and keyboard) rather than the processor and memory. Combining nano photonics, MEMS and electronics with recent UCSB work on Si nano wire thermal converters allows us to design a wafer that also has an embedded RTG or beta converter power source (recent LMCO work on thin film beta converters as an example) that can power the system over the many decades required in space. Combined with small photon thrusters (embedded LEDs/lasers for nN thrust steering on the wafer gives a functional spacecraft
originally posted by: chr0naut
a reply to: stormbringer1701
In answer to your final question, you could 'drop' a couple of relay transponders along the way.
You'd reduce mass with each drop off and create a semi-permanent comms network all the way to another star.
To my way of thinking, the real issue is how do you decelerate the probe?
Jade's "smart dust"would be great but not if it blows on by too fast.
well maybe something like an m2p2 for a star powered parachute? or actually the outward stellar wind even without an m2p2 parachute. but i think they actually have a complicated mirror system that allows then to invert the laser beam direction at the probe end.
originally posted by: chr0naut
a reply to: stormbringer1701
In answer to your final question, you could 'drop' a couple of relay transponders along the way.
You'd reduce mass with each drop off and create a semi-permanent comms network all the way to another star.
To my way of thinking, the real issue is how do you decelerate the probe?
Jade's "smart dust"would be great but not if it blows on by too fast.
originally posted by: JadeStar
originally posted by: chr0naut
a reply to: stormbringer1701
In answer to your final question, you could 'drop' a couple of relay transponders along the way.
You'd reduce mass with each drop off and create a semi-permanent comms network all the way to another star.
To my way of thinking, the real issue is how do you decelerate the probe?
Jade's "smart dust"would be great but not if it blows on by too fast.
Full Disclosure: My pet SETI project is one which looks to detect "someone eles's" smart dust in the near Earth and solar system environment. Shhh…. no paper yet
Mass and speed wkith 100 GW laser
1 gram 24% of lightspeed
10 grams 14% of lightspeed
100 grams 7.8% of lightspeed
1 kg 4.3% of lightspeed
10kg 2.4% of lightspeed
100kg 1.4% of lightspeed
1000kg 0.77% of lightspeed
10 tons 0.43% of lightspeed
100 tons 0.24% of lightspeed
originally posted by: Saint Exupery
Some quick calculations:
Assuming 50% efficiency (very high), to accellerate a 1 kilogram (2.2 pound) object to .25c would require
~8.333x10*14 Joules
which is equivalent to
231,870,000 KiloWatt-hours, or
834,000 GigaWatt-seconds
(Don't ask me what that is in pirate-ninjas)
The total energy-generating capacity of the United States is ~1,100 GigaWatts,
so it would take every single Watt of power produced in the U.S. for ~12 minutes 40 seconds
to accellerate 1Kg to .25c.
Ballpark figures, but it definitely gives you an idea of the magnitude of the task.
That is true...at least for now but (stolen from posterJohnSmith19 at NSF) :
originally posted by: 3n19m470
a reply to: stormbringer1701
At that speed, a 100 ton craft would take over 400 years to travel 1LY, if Im understanding this correctly.
Exhaust velocity for an Ion thruster c 30 000 m/s or 0.01% of lightspeed
Exhaust velocity for a fission fragment rocket 3-5% of lightspeed.
You can get right on that. meanwhile we'll get out the toolboxes and get building real hardware.
originally posted by: combatmaster
a reply to: stormbringer1701
all these technicalities just to traverse a few light years...
wouldnt it be easier to convert our conciousness into a form that we can manipulate and send ourselves anyhwere we want in the form of light?
originally posted by: Saint Exupery
Some quick calculations:
Assuming 50% efficiency (very high), to accellerate a 1 kilogram (2.2 pound) object to .25c would require
~8.333x10*14 Joules
which is equivalent to
231,870,000 KiloWatt-hours, or
834,000 GigaWatt-seconds
(Don't ask me what that is in pirate-ninjas)
The total energy-generating capacity of the United States is ~1,100 GigaWatts,
so it would take every single Watt of power produced in the U.S. for ~12 minutes 40 seconds
to accellerate 1Kg to .25c.
Ballpark figures, but it definitely gives you an idea of the magnitude of the task.