aspheric_cow

aspheric_cow t1_j4qjdtj wrote

Probably Texas or Mexico. If you go further north along the eclipse path, there is greater chance of clouds. Alternatively, be prepared to take a road trip to any part of the eclipse path, and decide a few days in advance based on weather forecast. Wherever you go, you want to be as close to the center of the total eclipse path as possible to get the maximum duration.

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aspheric_cow t1_j4l122v wrote

The aperture (size) of the telescope's main lens or mirror determines how much light it collects. If you use a high magnification, you are taking that finite amount of light and spreading it over a large image, so the image gets dim. This makes it difficult to see dim objects like comets. But if you use too low a magnification, some of the light is wasted, so for example, if you use 8x magnification on an 8-inch telescope, the view is no better than 8x50 binoculars. Worse actually, because you're only using one eye. So for viewing large diffuse objects, binoculars are ideal. If you can afford large astronomical binoculars (like 16x80) those are ideal, but even a common 8x42 works very well (and don't need a tripod).

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aspheric_cow t1_j4jx6yv wrote

Comets are large so you need a low magnification. Big telescopes can only work at high magnification - and also, cheap amateur telescopes are designed only for high magnification, because most people just look at the Moon and Saturn and that's about it. Binoculars usually have reasonable low magnification, like 8x to 12x. (Don't buy zoom binoculars that go up to very high magnification like 30x, those are trash.)

Comets are also dim and diffuse, and we can see dim objects much better if we use 2 eyes rather than just 1.

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aspheric_cow t1_j4iwcoq wrote

Hate to say this, but this isn't a very bright comet and there's nothing special about it. Your kid will no doubt have many chances to see brighter comets than this. So don't feel like you should put a lot of effort into viewing this one in particular. Save your money and put it towards a trip to see the total solar eclipse next year.

If you still want to try, as others said, contact your local astronomy club. Or see if any of your friends have good binoculars - maybe you know someone who is into bird watching?

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aspheric_cow t1_j477chf wrote

The power output does not scale linearly. The blades interfere with each other, so the more blades you put on a turbine, the less power each blade generates. Same reason nobody builds biplanes anymore - one long wing is more efficient than two shorter ones, one on top of another.

In fact, two blades would be more efficient (but less stable), and there are even examples of single blade turbines out there.

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aspheric_cow t1_j38aco0 wrote

Also, you want a larger nozzle at higher altitude (lower ambient pressure). An engine + nozzle optimized for low altitude would be very inefficient at high altitude, so you might as well drop it and switch to the high altitude engine. The Shuttle is an exception as you say, but actually the solid rocket boosters provided about 2/3 of the thrust at liftoff.

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aspheric_cow t1_j35n22k wrote

A faster ascent does take less energy - not because the gravity is stronger at lower altitude (the difference is pretty minor) but because the rocket spends more time fighting gravity. Think about the extreme case where the rocket is barely moving up - it will use up all fuel before it gets to any meaningful altitude. It's kind of like walking up a downward escalator - you have to expend energy just to stay in one place, and it's actually easier to run up quickly. Once you're at the top (in orbit), you can stay there without using any energy.

But there are limits on how quickly a rocket can accelerate, such as:

  • Quick acceleration requires more powerful engines. The engines themselves get heavier. This is mainly an issue with liquid-fuel rockets; solid fuel rockets don't really have an "engine" and you could design it to burn all the fuel very quickly if you want to.
  • The quicker you accelerate, the more G force & vibration the payload experiences. This is especially a problem if the "payload" is people.
  • If you accelerate hard, you end up traveling very fast through the dense low-altitude atmosphere, which means a lot of mechanical stress & vibration on the rocket.
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aspheric_cow t1_j1d7gxn wrote

One big disadvantage of solar thermal is that it doesn't work when it's cloudy. Conventional (photovoltaic) solar panels work fine with the diffuse light from an overcast sky, but you cannot focus diffuse light to create high temperature.

It's also mechanically complicated. Not only do you need a turbine (or Stirling engine) but you also need a tracking device to adjust the mirror angle continuously. Whereas conventional solar panels have no moving parts at all.

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