New Mars Forums

Official discussion forum of The Mars Society and MarsNews.com

You are not logged in.

Announcement

Announcement: This forum is accepting new registrations via email. Please see Recruiting Topic for additional information. Write newmarsmember[at_symbol]gmail.com.
  1. Index
  2. » Search
  3. » Posts by SBird

#426 Re: Interplanetary transportation » Photons have mass!! » 2004-03-18 21:18:27

Light in a black hole never actually stops.  As the photon falls into the singularity, relativity shows that time slows down for the photon.  Basically, the photon, from the viewpoint of the rest of the universe, never actually stops, it just keeps going slower and slower.  Therefore it never is actually at rest.

Of course, our modern physics could be wrong.  We already know that there are major problems with it because of the mismatch between relativity and quantum physics.  However, we KNOW that Newtonian mechanics which you are using for your assumptions is broken and badly broken at that.  You can't make statements like 'modern physics is srong, light has to have a rest mass'.  You can say 'light *might* have a rest mass', though.  It almost certainly doesn't, though.

#427 Re: Interplanetary transportation » Photons have mass!! » 2004-03-18 20:58:07

The movement of the high power calbe is actually due to the magnetic fields generated by large currents.  A current in a wire generates a circular magnetic field along the length of a wire.  This makes the wire jump.  I suppose that the electrons moving contributes to some extent but ti's a tiny amount.  Electrons have next to no mass and realyl don't flow that far in a wire.  I don't have the calculations handy but I recall that the eleactrons in the power main of an average house (ignoring the fact that the AC makes then move back and forth, just total motion) only move a few inches in a year.  The contribution of the electron motion is probably on the order of a drop of water compared to the Pacific ocean of the magnetic field.

#428 Re: Interplanetary transportation » Space elevator - breaktroughs predicted » 2004-03-18 20:53:26

Well in that case, where's my freakin' flying car!?  big_smile
I look at our war on cancer, AIDS, hunger, attempt to build an economical SST, LEO booster and I see a LOT of proposed engineering projects that never panned out.  It's easy to get lulled by Moore's law in semiconductors to think the same will apply to other fields.  However, Moore's law only works when you havea clearly defined engineering path to follow - in this case progresively shorter lithography wavelengths.

With CNT's, the formation mechanism is sort of understood and it doesn't look good, I'm afraid.  The problem is that youre trying to build flawless polymers.  The probability of a polymer getting longer without a flaw decreases exponentially with length.  Basically, if anything happens to the iron catalyst such as impurities or temperature changes or mechanical disturbances, the tube is killed.  The problem is that all of the nanotube synthesis schemes rely upon relatively high temperature synthesis where everything is kinetic in nature.  If we could find a way to get enzymes or simple organic precursors to make nanotubes, we'd be in business since then we could do things like error correcting, etc.  However, it's just not possible at the 200+C that anyone does the synthesis at.

Now, if someone were able to figure out a way to join nanotubes at the ends, we might just be able to do this.  It would require a supply of nanotubes of all the same diameter and chirality.  It mightbe possible to do this but the costs would be stupid staggering.  I mean just stupid. 

The big problem is that the elevator cable is so damn long and has to be so perfect.  One or the other is possibly feasible but both at the same time is really difficult.  The problem is that most other engineering projects can do just fine with the low quality tubes and so the massive effort to improve the CNTs has little economic incentive other than the elevator.  If the elevator requirements were just half as high as they are, I'd say that it's feasible.  However, the 100 GPa just requires such perfect material that I'm not terribly hopeful.

I can't rule out some major breakthrough busting the doors open but it would require a minor miracle in present day synthesis or a completely new synthesis method.

#429 Re: Interplanetary transportation » Photons have mass!! » 2004-03-18 16:08:50

Also, don't forget that a neutron isn't a particle - it's a collection of 3 quarks (2 down and one up, IIRC) that themselves have no volume.

Quantum physics is just wierd.  If you try and apply ideas like volume, momentum and other normal concepts to it, you just end up getting in trouble.  For example, in current physics models, mass itself is illusory.  It makes no sense from a common sense point of view but the equations seem to bear that conclusion out.  The same equations predict the behavior of the universe to 20 decimal places so they probably are at least partially true.

#430 Re: Interplanetary transportation » Photons have mass!! » 2004-03-18 16:03:18

SHOCK!  No pipeline?  Who are you and what have you done with ERRORIST!?  big_smile

OK, this is something that's a bit more practical.  I actually wouldn't bother with trying to accelerate the hydrogen.  If you're pushing a spaceship, all you have to do is shine a light out the back.  Since light has momentum, it will push you forward.   Now, all the stuff I mentioned about light being a very weak propulsive force still applies.

HOWEVER, this is actually the basis for a proposed propulsion system called a nuclear photonic drive.  Basically, it's a nuclear powered flashlight.  You have a nuclear reactor or some other endless power supply and use it to drive a super-powerful light source pointing out the back of your spaceship.

You have to have insanely powerful lights to make this work and have any sort of decent thrust.  On the other hand, though, the drive doesn't use any fuel.  Also, it uses light as the propulsive medium so you have excellent Isp values. 

Here's a wikipedia [http://en.wikipedia.org/wiki/Nuclear_photonic_rocket]link.

The drive would run until your reactor ran out of fuel which could be decades later.  This is the single best spacecraft propulsion system ever devised.  You only get a few pounds of thrust so you can't use it to get off the Earth but it would be an ideal drive for travelling to other star systems.

You wouldn't want to use a laser since lasers are VERY inefficient.  The most efficient way would actually probably be to just run the reactor core REALLY hot on the back of the spaceship at the focus of a parabolic mirror.  This way all of the visible and IR photons that are sent out as waste heat are used as thrust.  You approach efficiencies approaching 100% this way.  One problem is that the the reactor will slowly boil away at those temperatures.  However, if you use high temp ceramics and design the reactor so that it doesn't start boiling away down to the reactor core until the reactor is depleted anyway, this is not a problem.

The best part is that we could build this with present technology.

#431 Re: Unmanned probes » Europa » 2004-03-18 15:39:23

You're right that the mass won't be insignificant.  However, there's really no good way to send data through the ice itself.  It'll block light and radar and pretty much all other EM radiation at those thicknesses.  Perhaps ELF radio transmissions might make it but you'd need a super powerful transmitter to punch through.  The only way to communicate other than wire would be sonar but again you'd need a LOT of power to be able to be heard on the surface.  Perhaps with the nuclear power source they plan to have enough power to be able to do this but it seems questionable.  Also, both ELF and sonar have lousy data transmission rates.  You'd be waiting days to upload a single picture.

As far as cable, as long as you don't have to worry about the cable breaking (probably not a problem as it will be encased in ice), you can make it very thin.  In the Earth to LEO thread, I was talking about the idea of space tethers ( the rotating kind or electropropulsion kind, not the space elevator kind) with insane lenghts.  The tether I was using for a model was 100 km long but only weighed about 8000 kg.  That was for a tether that was impact reistant and could hold a weight of 3 TONS.  Check out Tethers Unlimited [http://www.tethers.com]here - that's where I got the data from.  They've got a nice site that explains things pretty well.

I'd expect that you could probably get a fiber optic info cable 20 km long that was a few dozen kg if you were careful.  Telecom fiber is about 0.3 mm in diameter without the protective covering.  Assuming a total thickness with protective sheath of 0.5 mm, that's a total of 0.002 cubic meters of material per 10 km.  A 50 km line, assuming you get about 50% packing efficiency (I have no idea how realistic that number is) it would all fit into a cube 27 cm on a side or about a cubic foot.  Pulling a density of 6 g/cm^3 completely out of my butt, the cable masses 59 kg.
Heavy but doable.

As for the concerns about radioactive contamination of Europa I saw in another post - it's non-issue.  Europa is already exposed to radiation levels from Jupiter's radiation belts that would kill a human on the surface in a few seconds.  While the ice stops most of this radiation, it is ridiculous to assume that none of it has made it into the interior over the last few billion years.  Also, the volume of Europa's oceans are estimated to be 10 TIMES the Earth's.  We released thousands of kilograms of radioisotopes in the 60's nuclear testing and failed to seriously hurt our ecosystems here.  20 kg of thermal radioisotopes in a shielded container area non-threat to a potential ecosystem of that size.  I'm much more worried about Earthly contamination hitching a ride on the probe.

#432 Re: Interplanetary transportation » Photons have mass!! » 2004-03-18 15:05:27

Well, it depends on how concentrated the beam is, how well the wavelength coupled to H2 absorbtion, how long you hit the atoms with the light and so on. 

For individual atoms, using a laser is a very inefficient way to push them around.  In fact, with a regular gas, you'll just heat the gas up.  This is because the atoms will bounce off each other and soon, their velocity vectors become randomized.  You'll only get significant velocity if the gas is extremely thin.  By thin, I mean molecular flow regime which starts at about 1 billionth atmospheric pressure. 

So, to answer the question you were about to ask, a laser would push hydrogen up your pipeline - but very poorly and only if you had pretty much no hydrogen in it.  You'd get more H2 to orbit if you built a ladder and had a guy carry buckets of the stuff up to orbit by hand.

#433 Re: Science, Technology, and Astronomy » Question about rockets & thrust » 2004-03-18 14:50:10

Oh yeah, you might also be interested to note that the Saturn V had a larger cargo mass fraction that most modern launch systems despite its lower performance. 
For example, the Shuttle has a higher total mass fraction (being defined as the mass of the spacecraft that gets to orbit vs the total mass including fuel that it starts out with) than the Saturn V.  However, the Shuttle wastes most of this on things like wings and carrying heavy engines to orbit, etc.  As a result, the Shuttle can barely manage a cargo mass fraction of 1.5%.  That means that of the total mass of the Shuttle, esternal tank and SRBs ar launch, 1.5% of that is actual satellite cargo.  All of the rest of the extra mass is flown back down to Earth - how wasteful!
The Saturn V had a cargo fraction of 3%.  This is because it was basically a set of minimal fuel tanks with some cargo strapped to the top - nothing was included in the launcher that wasn't strictly necessary. 
This is why I'm a big proponent of scrapping the Shuttle and going back to the old big disposable booster style of doing things.  Done properly, it's a lot cheaper.

#434 Re: Science, Technology, and Astronomy » Question about rockets & thrust » 2004-03-18 14:42:58

The O2 and kerosene were stored in seperate tanks like O2 and H2.  A premixed mixture of oxidizer and fuel would be insanely dangerous.  A mixture of fertilizer and fuel oil is a much less energetic fuel/oxidier mix and we all got to see what even that did in OK city.  Plus, kerosine would probably solidify at liquid O2 temperatures.  The two were mixed either right before or in the engine combustion chamber.  IIRC, the liquid O2 was sent through tubes in the engine cones to keep them from melting and to preheat and pressurize the O2.

The golden color most definately from the kerosene. (most likely more highly purified than camp stove stuff but basically the same)  O2/H2 burns hotter and cleaner so it gives this tiny little blue flame.  The Shuttle main engines generate thrust levels comparable to the F-1s, IIRC but you can barely see the flame.  O2/H2 is a much better fuel but you're right, the gold kerosene glow was much better looking. big_smile

I know that at least one X-prize competitor is using O2/kerosene since kerosene is much cheaper and easier to handle than H2.

#435 Re: Science, Technology, and Astronomy » Lots of (mostly) science questions » 2004-03-18 14:36:06

LEO isn't a fixed value, either.  I think it ranges from about 250 km to 500 km.  I have 7814 m/s as the lowest delta V that will get you to a stable orbit.  (I assume that this is an orbit that only lasts for a few hours due to atmosapheric drag.)

#436 Re: Science, Technology, and Astronomy » NASA & Voice-Recognition Software » 2004-03-18 14:34:13

I dunno, I've seen how well regular voice recognition works and I'd be terrified if my life depended upon it.  I remember an old roomate got some free voice recognition softwre with a sound card.  It was one of the better commercial packages at the time (Somthing-or-other-Dragon or something was the name).  I just remember hearing him in his room saying:
"Emergency."
"Undo...Undo"
"Emmmmergency"
"Undo...Undo...UNDO"
"EmergEEEncy"
"Undo...undo"
"EEEmergencYYY"
"Undo...Undo...Undo...UNDO!!"
And so on for about 10 minutes.

Later, after he'd finally programmed the dumb thing, my other roomate anda friend were testing it out.  I can't remeber what someone said but the program interpreted it as "Robber the condom."  The resulting laughter caused the program to write a long paragraph of "Whom"s....

#437 Re: Science, Technology, and Astronomy » Lots of (mostly) science questions » 2004-03-18 14:28:55

I haven't seen any hard numbers for the X-prize delta V but I was under the impression that is was something like 1/11th  the delta for LEO.  That would put it at something like 0.5 km/s. 
This is why most of the schemes like maglev boosters and such don't work well.  Almost all of your energy is spent up above the atmosphere going horizontal and getting enough centripetal velocity to keep from falling back down.

#438 Re: Interplanetary transportation » Earth to LEO - discuss » 2004-03-18 14:19:53

The situation I was thinking of is the future where we're launching large numbers of rockets off to Mars on a regular basis.  That justifies the fixed orbital inclination.  If the launcher costs $10 billion to manufacture and $100 million a year to run, saves 20% of the $500 million a launch per rocket costs, it could end up being a net money saver in a decade.

A space elevator would be the best bet but read one of my messages on the boards here to see what I think of the probability of that happening anythine soon...

#439 Re: Unmanned probes » Spirit & Opportunity*4* - continue here » 2004-03-18 14:05:43

Mossbauer spectroscopy is one of the wierder ones.  I don't fully understand how they get the electronic structure out of the nuclear energy levels but here's an explanatory link: [http://www.rsc.org/lap/rsccom/dab/mossb … /intro.htm]link

#440 Re: Unmanned probes » Rosetta - ESA comet orbiter and lander » 2004-03-18 14:02:07

I think that this sort of tech is most useful in exploring the moons of Mars.  It's a way to land on an object with minimal gravity where the probe is likely to float away unless anchored down.
I'd love to see a probed investigate the moons of Mars directly.  There's all sorts of potential uses for the moons that would be made possible by a better understanding of them.

#441 Re: Unmanned probes » Europa » 2004-03-18 13:50:39

I think that's how it's presently envisioned.  Basically, imagine tying a string to a tree and walking away with the spool.  Even though the string behind you stays still, you can just keep playing out the string as you walk along. 

In this case, the wire left behind is refrozen into the ice which probably actually increases the longetivity and lifetime of the wire.  10 km of thin wire isn't too big of a challenge.  (in fact, I think that fiber optic would be the way to go for good data transmission.)

#442 Re: Interplanetary transportation » Earth to LEO - discuss » 2004-03-18 13:45:29

I think that the prolems of building on the PAcific ocean and dealing with the foothills are child's play compared to building a precision, large structure on a mountain.  I've done mountain climing in the past and it is NOT a friendly environment to anything more involved than a hut or a gondola tower.  The Andes do seem more promising.  I suppose that a 50 degree launch angle might even be possible for some of those peaks.

Assuming that we can build the track in that kind of envorinment and the first avalance doesn't wipe the track away, what sort of numbers are we looking at?

Well, since we've pretty far into the future with being able to build this mega track, lets assume that we can go supersonic.  Soem of those Andean peaks can top 23,000 feet.  Let's assume you get a launch angle of 50 degrees at a launch velocity of mach 3.  You've got a vertical velocity of about 785 m/s which is about 10% of the total delta V needed.  I'd say that this might be worth using.  You've still got to carry a lot of weight to space but it wil help. 

Assuming an H2/O2 launcher and ignoring air drag, this launcher give you about an 23% increase in the cargo capacity of the rocket.  Not stupendous but measureable.  To double your launcher capacity, you've got to have atotal vertical velocity of 2420 m/s or 5413 mph.  At a launch angle of 50 dergrees, you need to lob that rocket at mach 9.5.

I don't think the equations I'm using take things like staging into account properly so you could probably improve those numbers quitea bit.

However, it remains that a maglev launcher is an incremental launch improver.  It won't give you 10-fold decrease in launch cost.  THe differences will be measure in percent.  It may well be a vialbe option someday but I think that we need to have a much more crowded launch schedule to justify the contruction of something like this.

#443 Re: Science, Technology, and Astronomy » Lots of (mostly) science questions » 2004-03-18 13:15:36

Some excellent questions.  I'm afraid that I'm not qualified to answer most of them but I'll give it a shot.

1: You are correct in that cost doesn't scale linearly with launch mass.  On one side, many costs like engines and the like actually get cheaper as you go up in launch mass.  However, other things like the launch facilities and fuel tanks and the like get almost exponentially more expensive with increasing launch mass.
Furthermore, you can kep the same launch mass and dramatically reduce cost by smarter engineering.  NASA and other space agencies tend to forget the KISS principle and it costs us a lot of money.  For example, the Boeing Sea Launch platform can deliver as much to LEO as an Arianne 4.  Despite being similar in launch capability, the Zenit is half as expensive (~$2500/lb vs ~$5000/lb) to operate.  A large part of this is that the actual fuel costs of a rocket are something like %1.5 of the total lauch costs. Likewise, the physical rocket is a minor part of the cost.  The big cost is the army of people needed to fly these things.  Sea launch uses a really simple launcher that requires a minimal number of technicians to operate. 
A similar philosophy is going on at SpaceX.  I'm not qualified to say whether the numbers are correct but this company is claiming that they will be able to get launch costs down to $1000/lb.  The technology they are using is primitive but simple and cheap.   I think that this philosophy is important.  To get to Mars, we don't need fancy launchers, we need to look at the bottom line - how cheap can we get a reliable 140 ton to LEO booster?

2: not qualified to answer this myself but the atmospheric drag is a fairly small portion of the total delta V.  Most rockets clear the lower atmosphere in a minute or so.

3: The X Prize really isn't an orbit any more than a thrown baseball is.  As for the other orbits, most stuff is in LEO since it's cheap to get to.  However, satellites sit in all sorts of orbits.  For example, the GPS sattelites sit somewhere between LEO and GEO where they orbit the Earth about every 12 hours, IIRC.  You should be able to get relevant delta Vs from a Google search.

4: I think most engineers have gone over to metric these days or should have.  I'm not a rocket engineer, though so I don't know what the state of the industry is.

5: Gravity doesn't affect the system in any way tat a competent chemical engineer couldn't deal with on paper.  The only process I can think of is the gass flow rates through a condenser if it's being driven by buoyancy of the entrant gas.  However, I think that the whole system is pump driven so it should work in zero G.
Dust is more of a problem but there's plenty of dusty environments on Earth that we've managed to engineer for. At present, I think that refrigeration is the planned system for getting CO2 and so a simple subicron filter could be used to screen out dust.  Plus, I don't think that anything other than the pump is too severly affected by dust in the ISPP setup.

6: most of the Martian metorite evidencee was debunked.  However, there is still quite a bit of controversy about the magnetite particles in the meteorite.  There's a camp which I tend to side with (being familiar with the field of study), which posits that the magnetite particles look liike they are biologically derived.  However, the best analytical labs on Earth haven't resolved this problem.  I don't see Martian probes or expplorers being able to do much better unless they find something much more conclusive.

7: If anythingI think that our terraforming estimates are even fuzzier with the newer data coming out.  There's a lot of stuff we don't know about how Mars behaves over extended periods of time.  Evidence seems to indicated that Mars was a lot warmer in the recent past. (like within the last 3 million years)  It could be that Mars has major climactic oscillations and that it has frequent warm periods.

8: Dont know enough about the details of the new MArs plan to comment.

9: Don't know.

10: Sorry.

11: I don't know but since a full time lobbyist would probably cost at least $150,000 a year, I doubt the Mars Society has oone.

12: Not to my knowledge but this isn't a bad idea.  I'm not sure how much sense you can talk into those groups but the situation certainly going to improve if we don't at least try and communicate with them.  I think that a lot of members of those organiations are reasonably minded but misinformed.  A litle correct info could go a long way.

#444 Re: Interplanetary transportation » Photons have mass!! » 2004-03-18 12:41:57

It depends on what wavelength of the light is.  Hydrogen will only absorb light of certain, specific frequencies.  (hence why spectroscopy works).  The absorbtion of a single photon will give some momentum to a hydrogen atom.  The higher the frequency, the greater the momentum transferred.  I don't have any numbers handy but it won't be much.  You need a LOT of light to be able to generate any meaningful light.  That's why you can't use a flashlight to fly around. 

Solar sails can generate thrust by using light.  The best situation is to use a reflective surface. Basically, reflective materials like metas have loosly bound electrons that kinda of float around like an electron gas, not particularly bound to one atom.  (it's why metals are conductive)  When light hits, the elecrical component causes a reciprocal oscillation in the electron dentisity that basically causes the photon to 'bounce' off.  It's kind of like a rope that's attatched to a wall with a spring - if you give the rope a twitch to send a wave down its length, the wave will bounce back off the spring.

In this fashion, the photons are bounced backwards.  So not only do you get the momentum of the light hitting the object, you also get the momentum of the photon being redirected in the oposite direction - you've just doubled your thrust.  Even so, at the Earth's distance from the sun, a sail with an area of a square kilometer generates about 1 kg of thrust.  It's pretty weak.  The big problem with solar sails, is that in order to get enough thrust, you need a HUGE sail and the mass of the sail adds so much weight to a spacecraft that it takes forever to get anywhere.

#445 Re: Interplanetary transportation » Photons have mass!! » 2004-03-18 12:28:39

No, a photon has no rest mass since it can never be at rest.  Trying to apply standard Newtownian physics to a quantum mechanical concept makes about as much sense as trying to measure speed in liters.  The standard mass-kinetic energy equations you are familiar with are wrong.  For macroscopic objects, they have been replaced with relativistic equations (which, for everyday objects ends up being almost exactly what Newtonian mechanics predicts) and small particles are governed by quantum mechanics which is a completely different ball game.

Reconcilling the world of the small and large is one of the greatest problems in science.  Some recent experiments in quantum decoherence are starting to shed light on the problem but we are still a long ways away from understanding what's going on.

#446 Re: Interplanetary transportation » Photons have mass!! » 2004-03-18 12:23:34

Actually, that answer isn't really correct.  The polarization of light has nothing to do with how wide it is and its ability to pass through a given space. 

Polarization occurs because light can be thought of as an oscillating electric field at a right angle to an oscillating magnetic field.  In linearly polarized light, both the electric and magnetic component are also ata right angle to the direction of travel.  (imagine two sine waves at right angles to each other - the long axis of the travel is the direction the light is going.)

Polarizing materials have a net imbalance in how easily they intereact with an oscillating magnetic field.  This is due to the crystal structure.  Most crystalline materials exhibit this behavior to some extent.  Materials that act as polarizing filters simply exhibit this property to a greater extent. When light hits a polarizing filter, the electric field interacts with the material depending upon the angle it hits at.

As far as the 'size' of light, it's a poorly phrased question.  elementary particles don't really have a size as we know it.  a photon has a size of 0.  A light wave in the visible range has a size of about half a micron.  The currently accepted model (which is likely to be at least partially wrong) is that the wave nature of light is in the form of a probability wave that takes on the form of a photon when it interacts with another particle.  The probability wave simply is the proability distribution of where that interaction is likely to take place.

#447 Re: Unmanned probes » Europa » 2004-03-18 12:12:27

I think that the idea for a umbilical cable is that it feeds off a reel on the back of the probe so that when it gets frozen into the ice, it's no big deal. 

As for ultrasound or sonar, the projected thickness of the ice is much too thick to be able to penetrate unless you're using nukes or something to generate the sound.

#448 Re: Interplanetary transportation » Photons have mass!! » 2004-03-18 12:06:22

I'm almost afraid to ask, but why do you think that the books are wrong?  It's an established fact that photons have mass, otherwise they couldn't transfer momentum.  They have no rest mass which is fine since they never stand still.

#449 Re: Unmanned probes » Mars Science Laboratory (MSL) - rover » 2004-03-18 12:02:13

I might have missed it in the discussions above, but it seems that no one's mentined the fact that this rover will be RTG powered.  This is a significant step forward, IMO for a rover.  Instead of a 90-day rover that ends up running 6 months, we can expect to be able to get observations for a few years.  Also, the massive increase in the number of scientific instruments is a welcome change.  In some ways, the present rovers area disappointment since they really don't compare too favorably to the Viking landers 27 years ago. 

I'm glad to see that a life detection setup is being planned again.  The life detection chip is pretty ingenious, it replaces an HPLC with a mass of a couple of grams.  I'm guessing they're probably using something like [http://www.probes.com/media/pis/mp02333.pdf]this for the amino acid detection.

Hopefully, someone can get them to shoehorn a miniature ISPP setup to at least test fuel production in an actual Martian environment.

#450 Re: Interplanetary transportation » Nuclear, Pro & Con » 2004-03-18 10:30:02

I'm glad to see the Navy getting on board here.  They have the best safety record in the world with nuke reactors.  I know a guy that was in the nuke program when he was in the Navy - the school has something like a 95% dropout rate.  They're pretty unforgiving to candidates and toss anyone who shows the slightest sign of not being competent.

  1. Index
  2. » Search
  3. » Posts by SBird

Board footer

Powered by FluxBB