Near solar mirror for beam propulsion and space solar power

In summary, NASA is launching a solar probe named after solar astrophysicist Eugene Parker, who predicted high speed solar wind. The probe will travel about 3.7 million miles from the solar surface and has the potential to collect a terawatt worth of power at that distance. This power could potentially be used for space solar power when beamed towards Earth. However, the temperature at this distance is around 1,400C and a high-temperature reflector, such as tungsten, would be needed. A more optimal distance for collecting solar power may be closer to Mercury, at about 7.5 times further out than the Parker Solar Probe's location.
  • #1
RobertGC
89
2
NASA just announced a solar probe to travel quite close to the Sun, about
3.7 million miles from the solar surface:

Nasa’s hotly anticipated solar mission renamed to honour astrophysicist
Eugene Parker.
Renamed the Parker Solar Probe to honour solar astrophysicist who predicted
high speed solar wind, the spacecraft will attempt to get close to sun’s
surface.
Wednesday 31 May 2017 07.08 EDT
https://www.theguardian.com/science...ticipated-mission-to-the-sun-solar-probe-plus

Spacecraft able to get this close to the Sun could potentially allow beamed
interstellar propulsion. For a spacecraft of any size, you would need huge
amounts of beamed power. Where to get it? If you make the beam be
solar-powered then can just use space-borne mirrors to focus the Suns rays.
But the mirror(s) would have to be impractically large if they were in Earth
orbit.

But what if we placed them close to the Sun? At the distance quoted of 3.7
million miles away from the Sun a mirror 1 km on a side could collect a
terawatt worth of power.

Note this could also be used for space solar power when beamed towards
Earth.

What would be the size of the collector array at Earth to capture most of
the light focused from the 1 km wide mirror located at the Sun, i.e., the
size of the Airy disk at the Earth? How large at Proxima Centauri?

Bob Clark
 
Science news on Phys.org
  • #2
RobertGC said:
3.7
million miles away from the Sun a mirror 1 km on a side could collect a
terawatt worth of power.
What temperature would it need to be operating at? Is there any know refractory material that's also a good reflector?
Perhaps a happy medium distance would be better to aim at? Somewhere a bit closer than Mercury, say 4AU.[Edit: that's about 0.3AU]
 
Last edited:
  • #3
sophiecentaur said:
What temperature would it need to be operating at? Is there any know refractory material that's also a good reflector?
Perhaps a happy medium distance would be better to aim at? Somewhere a bit closer than Mercury, say 4AU.

An AU is an "astronomical unit". It stands for the distance from the Earth to the Sun. So you want the distance to be a fraction of an AU. By wikipedia, Mercury is at about 46 million km from the Sun. This is about 7.5 times further out than the Parker Solar Probe is supposed to be. The intensity of the solar light will be decreased by the square so will be 56 times weaker than at the location of the Parker probe.

The temperature is cooler though at Mercury at about 430C compared to 1,400C at the Parker probe location.

For a high temperature reflector you could use tungsten.

Bob Clark
 
  • #4
Owch. That's what comes from trying to use an iPhone. I missed out the 0.0! Sorry and well spotted.
 

1. How does a near solar mirror work for beam propulsion?

A near solar mirror is a type of solar sail that utilizes the sun's energy to propel a spacecraft. It consists of a large reflective surface that reflects and concentrates the sun's rays onto a small area of the sail, creating a powerful beam of light. This beam of light exerting pressure on the sail provides thrust and propels the spacecraft forward.

2. What are the advantages of using a near solar mirror for beam propulsion?

One advantage is that it does not require any onboard propellant, making it a more efficient and cost-effective propulsion method. Another advantage is that it can continuously accelerate a spacecraft, unlike traditional rocket engines that have limited fuel. Additionally, it can reach very high speeds, making it ideal for long-distance space travel.

3. Can a near solar mirror be used for space solar power?

Yes, a near solar mirror can also be used for space solar power. The same technology that allows it to reflect and concentrate sunlight for beam propulsion can also be used to collect and transmit solar energy back to Earth. This can provide a sustainable and renewable source of energy for our planet.

4. What are the challenges of using a near solar mirror for beam propulsion and space solar power?

One challenge is the precision required for the mirror to reflect and concentrate the sunlight accurately. Any slight error can result in the beam missing the sail or the solar energy not being effectively collected. Another challenge is the potential damage to the mirror from micrometeoroids and other debris in space.

5. Are there any current projects or plans for using near solar mirrors for beam propulsion and space solar power?

Yes, there are several ongoing projects and plans for utilizing near solar mirrors for beam propulsion and space solar power. Some examples include NASA's Sunjammer mission, the Breakthrough Starshot project, and various space-based solar power concepts proposed by companies and researchers. These projects and plans are still in the early stages, but they show promise for the future of space exploration and energy production.

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