Truth.You mis-spelled Babylon 5.![]()
Truth.You mis-spelled Babylon 5.![]()
I've taken a closer look at how much velocity change (delta V) is needed to get into low Earth orbit. I used the Saturn V rocket's performance, and I calculated a delta V of 9.5 km/s for getting into LEO. That's more than the 8.0 km/s Hohmann transfer orbit from the surface to 170 km, its LEO altitude. The difference is 1.5 km/s, and that's due to overcoming the Earth's gravity.
Let's now consider larger planets. Planet Models shows the smaller exoplanets with both mass and radius known. Even the lightest and smallest of them is still more massive and larger than the Earth. Up to about 3 to 3.5 Earth masses, they are all rock-iron, much like the Earth itself, but there are only 2 or 3 planets in that sample. But more than 3 or 3.5 Earth masses, some of the have lots of volatiles, especially hydrogen and helium, though some others still have densities consistent with Earthlike compositions.
I'll now use some structure calculations that exoplanet searcher Sara Seager and some others have worked on. For 3.5 Earth masses and an Earthlike composition, the radius is about 1.33 Earth radii (this model gives 0.97 Earth radii for 1 Earth mass). Its surface gravity is 1.98 times the Earth's, and its surface-satellite orbit velocity is 1.62 times the Earth's, or 12.8 km/s. That's 4.9 km/s more than the Earth's value of 7.9 km/s, and that increase is half the LEO delta V.
I estimate that the likes of the Saturn V and the Falcon 9 have close to a 20:1 mass ratio for (initial mass) / (LEO payload mass), and scaling it up means taking 20^(3/2) or 90. That means that one can put into low orbit only 1/4.5 times the mass that one can put into LEO, with the same initial rocket size. One will need an additional rocket stage, I think.
It's all still perfectly dooable, but they'd have to put a lot more thought into how they did it. The shuttle would have to descend far away and then fly a long way at treetop level to avoid detection.I do like the suggestion that the Captain's Yacht or the Aeroshuttle would have been used commonly. That makes more sense. Of course, that's nothing more than just another type of shuttle. You are facing a limitation of stealth with a shuttle. Landing a shuttle on many of the planets we saw on Trek would have violated the Prime Directive.
Well the Doomsday Machine one is pretty simple: instead of a transporter, they're trying to escape on Constellation's one remaining shuttlecraft, and it's so badly damaged that they can barely get the engine working in time to get off the ship. So the big dramatic moment, instead of scotty trying to get the transporter working, you have Kirk running into the hangar deck to find the shuttle's engine on fire and Scotty and/or Chekov desperately trying to get the thing working in the 30 seconds they have left before Constellation goes down the tube. They finally get the engine started and bolt through the shuttle bay at the last minute and only BARELY outrun the explosion.And the quick escapes would have to be reworked. No beaming Kirk out of the Constellation at the last second before exploding inside the Doomsday Machine. They would have had to dig Data up after he was buried in Thine Own Self.
That's not true at all. Actually, the best high-exhaust-velocity engines we have only work in an atmosphere. Ramjets and scramjets being the primary examples of these: they are capable of fairly high exhaust velocities but ONLY for a craft already traveling at very high speed through an atmosphere. Scramjets are (theoretically) even competitive with the best rockets we have, but again, hindered by the fact that they only work when they have air to suck down.From Tsiolkovsky's rocket equation, to consume less propellant, one needs greater exhaust velocity. But to get off a planet, one needs enough thrust to counter the planet's gravity. To date, it has been difficult to have both. There is the further problem that most existing high-exhaust-velocity engines only work in a vacuum.
The low thrust from ion engines is purely a function of their power input. The extent to which ion engines are scalable to higher power outputs is not VERY well understood, but we know there are some limitations that good design can account for.One can get much higher exhaust velocity with alternatives like ion engines. Dawn's do 30 km/s. But Dawn's engines have very wimpy thrust. Each of the three has a thrust of 90 millinewtons. In fact, the spacecraft's rocket engines were "on" for much of its travel time.
That's only if it has the same column density, mass per unit area. Since (pressure) = (column density) * (gravity), it will go up. But if a planet has less atmosphere, then its surface pressure and density could be around ours.Are you taking into account changes in atmospheric density as well? Higher gravity means the atmosphere will be pulled in closer to the surface, making it more dense, meaning that you've got more drag to deal with in addition to more gravity to fight. That should reduce atmospheric delta-v fairly significantly as well.
That's only if it has the same column density, mass per unit area. Since (pressure) = (column density) * (gravity), it will go up. But if a planet has less atmosphere, then its surface pressure and density could be around ours.
The higher gravity has an interesting consequence: the planet's atmosphere would fall off more rapidly with height: (fall-off distance) ~ 1/(gravity).
I note that a higher acceleration of gravity has additional effects, like making mountains lower and inhabitants shorter -- (height) ~ 1/(gravity).
The square-cube law? That might work, though it may be hard to outgas from anything deeper than the crust and uppermost mantle.But considering the source of the atmosphere, a larger planet should, if anything, have more atmosphere than Earth, not less, shouldn't it? More total mass to begin with, so there'd be more vapor to outgas during planetary formation.
The square-cube law? That might work, though it may be hard to outgas from anything deeper than the crust and uppermost mantle.
But it must be noted that that is a big unknown. We don't know for sure whether Earthlike planets tend to form with about as much volatiles as the Earth has, whether they tend to form with much more, making ocean planets, or whether they tend to form with much less, making desert planets -- or whether they can form with a big range of volatiles.
“The total H₂O content of the planet has long been among the most poorly constrained ‘geochemical parameters’ in Earth science. Our study has found evidence for widespread hydration of the mantle transition zone,” says Jacobsen.
That tells us exactly nothing, since we don't have a reliable way to estimate its abundance in the Earth's mantleThere is a weird issue with uranium. U-238 has a half-life of 4.468 billion years, about the Earth's age. U-235 has a half-life of 703.8 million years, much less. U-235 is about 0.72% of the uranium in the present-day Earth's crust
That also doesn't mean anything. The distribution of 238 to 235 would depend entirely on what the ratio originally was to begin with. If the early mantle had a much higher proportion of the former than the crust, the proportions will still be higher today. That's just the way half life works: the heavier isotope decays over time, but SINCE it takes a predictable amount of time, the only variable is actually the starting conditions, which we really have no way of knowing.I seriously doubt that there has been much fractionation of uranium isotopes in the Earth's crust. They are chemically the same and their atomic masses are not very different.
Why? Again, you have no way of establishing whether or not these really WERE the initial conditions, let alone whether or not alpha or beta decay were their only behaviors at this point. On the one hand, forming closer to the sun than most of the rocks of the belt or even the wandering NEOs means the proportion of heavy metals could easily be much higher, favoring uranium more strongly than in the outer solar system. On the other hand, there are circumstances where even uranium 235 can reach critical mass NATURALLY and can undergo spontaneous fission into lighter elements, in which case the initial conditions could be dramatically different than that found in modern day asteroids. Other radioactives and secondary decay products also produce heat and have their own critical masses that could potentially be reached under the high pressure and density of the lower mantle. We have virtually no reliable data about what's actually happening down there, let alone what was happening 4 billion years ago.I'll set the Earth's present U-238 to 1. The abundances of U-238, U-235, and Th-232 are thus (1, 0.0072, 2.6).
That, again, is not something you have any way of saying with confidence. A planet generated from a third or fourth generation star might actually have little or no uranium at all because criticality events in the cores of ancient planets broke it down into lighter elements early on. Or it might have a stupendously high abundance of it due to the influence of another gravitating body creating a mass sink for the heaviest elements. There are too many variables in this -- and also too many unknowns BY FAR -- to attempt to make the kind of predictions you're making.Now for a planet that formed when our Galaxy was only a billion years old. The Earth started out with abundances of (U-238, U-235, Th-232) = (2.03, 0.64, 0.49).
That would require some extreme isotope fractionation.That also doesn't mean anything. The distribution of 238 to 235 would depend entirely on what the ratio originally was to begin with. If the early mantle had a much higher proportion of the former than the crust, the proportions will still be higher today.
There is an indirect way of checking. Comparing ages measured with different radionuclides. U-238 and U-235 and Th-232 and K-40 ages ought to show systematic discrepancies. But we don't see any evidence of that. Furthermore, the radiometric-dating ages of the oldest Solar-System material agree with the age of the Sun derived from helioseismology interior probing and stellar-evolution calculations.Why? Again, you have no way of establishing whether or not these really WERE the initial conditions, let alone whether or not alpha or beta decay were their only behaviors at this point.
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