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Guest Message © 2012 DevFuse

D H's Profile User Rating: -----

Reputation: 1088 Glorious Leader
Group:
Resident Experts
Active Posts:
3,208 (1.43 per day)
Most Active In:
Politics (426 posts)
Joined:
30-March 06
Profile Views:
8,204
Last Active:
User is offline Yesterday, 11:53 PM
Currently:
Offline

My Information

Member Title:
Physics Expert
Age:
Age Unknown
Birthday:
Birthday Unknown
Gender:
Not Telling Not Telling
Location:
Houston, Texas
Interests:
Now that my kids are grown up and out of the house I will have time for some hobbies
College Major/Degree:
Physics, during the stone age
Favorite Area of Science:
Spacecraft guidance, navigation, control
Biography:
w*h*a*t*i*s*s*i*x*t*i*m*e*s*n*i*n*e
Occupation:
Aerospace engineer

Contact Information

E-mail:
Click here to e-mail me

Posts I've Made

  1. In Topic: Ion Drive

    23 May 2012 - 01:49 PM

    View Postthe asinine cretin, on 23 May 2012 - 09:13 AM, said:

    The more I look into them the more intrigued I am by stirling radioisotope generators. The tech exists and has demonstrated to be both significantly more efficient and lighter than RTGs; at least according to the stuff I've been reading. There is a big push to finish its development.

    The main driver behind that push is the fact that domestic production plutonium 238 has been shut down since 1993. Funding to get that domestic production restarted is barely there, and it's only on the NASA side. Producing 238Pu the job of the Department of Energy, and Congress for some reason refuses to fund the DOE side. Logjam.

    If there was an adequate supply of plutonium 238 NASA would happily continue using RTGs. They are a very simple and very trusted technology. No moving parts. They don't fail. While much more efficient, those Stirling generators are new technology and are significantly more complex than RTGs. Increased complexity means a significantly increased likelihood of failure. That it is new also increases the risk of failure. A lot.

    The ASRGs will be used for low power consumption devices such as sensors and communications. Using them for a high power consumption device such as a VASIMR engine is not going to get a vehicle to Mars. At least not very fast. Do the math. A VX-200 sucks 200 kW of electrical power, or the output of 1400+ ASRGs. At 32 kg per ASRG, the power source needed to supply a VX-200 masses over 45,700 kg. That's just for the power source, not the housing for those 1400+ units or the electrical cable needed to connect them to the engine. All for 5 newtons of thrust.
  2. In Topic: Ion Drive

    23 May 2012 - 07:14 AM

    View Postthe asinine cretin, on 23 May 2012 - 04:58 AM, said:

    In other words you don't know?

    No news is most often bad news when in comes to companies that delve into new technologies. Or it might mean they are quietly working on things where progress is measured in years. Many, many years in this case.


    Quote

    Right. I was only talking about the fuel and not infrastructure. But I wouldn't call thermocouples "extremely massive infrastructure." There are things to consider beyond just the fuel? No kidding, everyone knows that. Perhaps you mistook this for a formal proposal. lol. Condescension isn't the reply I was hoping for.

    There's a lot more to RTGs than thermocouples, particularly an RTG that contains 100 billion lethal doses of 210Po. The fuel is encapsulated in ceramic, surrounded by iridium, which in turn is surrounded by high-strength carbon, which in turn are placed in housings, which in turn is surrounded by an aeroshell. There is a whole lot more to an RTG than just the fuel and a couple of thermocouples.


    Quote

    You evidently missed my comments about efficiency. Based on modern RTGs I suggested 7% as a reasonable efficiency but later mentioned a contemporary prototype device that is said to attain 30% efficiency. Since I'm freely speculating about what's possible, and not trying to be cynical, I think it's okay to imagine what could be done with a 7-30% efficient system.

    Those higher efficiency systems are not RTGs. They are heat engines. Now you have a working fluid, moving parts, a heat exchanger, a generator, and you still need massive amounts shielding to keep those 100 billion lethal doses from escaping in case of some kind of accident. There's a good reason that none of the world's space agencies have gone to these speculative devices. The four fold boost in efficiency is not worth the added mass.


    Quote

    Moontanman's interpretation is correct. Obviously the radioisotope would be manufactured in situ on Mars.

    Obviously not. Where does it come from? That in situ manufacturing would require building on Mars an automated bismuth mine, an automated bismuth refining plant, an automated nuclear reactor, an automated neutron bombardment facility to bombard the mined and refined bismuth with neutrons, an automated purification system to isolate the polonium, and an automated storage system. It's ludicrous.
  3. In Topic: Ion Drive

    22 May 2012 - 07:22 PM

    View Postthe asinine cretin, on 22 May 2012 - 05:00 PM, said:

    Interesting. Has anything changed since 2010? As I mentioned in another thread, Ad Astra says that the VASIMR is to be tested on the ISS in the near future. I've not seen any substantial details.

    No news is no news. Or in some cases, it's bad news. Lots and lots of proposed technologies start with a flourish but then just fade away.


    Quote

    A two inch cube of polonium-210 would emit 140kW. That could definitively get you many kilowatts per kilogram; perhaps the two orders of magnitude you desire when compared with your numbers. The half-life is less than five months but I imagine a very compact and light weight RTG could power a VASIMR on a robotic spacecraft and ramp it up to extreme speeds for outer solar system recon and the like.

    What you are doing here is accounting for the mass of the fuel but failing to account for the mass of all of the infrastructure needed to make that fuel useful. The decay of polonium 210 generates heat. VASMIR runs on electricity. You are ignoring the fairly massive infrastructure needed to convert that heat into electricity plus the extremely massive infrastructure needed to ensure that the PO-210 remains safely encapsulated even in the case of an explosion. That alone changes your many kilowatts per kilogram into many kilograms per kilowatt. Then there's the problem of the efficiency of that conversion of heat into electricity. RTGs are simple devices with no moving parts. The downside: They are extremely inefficient. Typically efficiency is about 5%. Your two inch cube of polonium-210 would generate about 7 kW of electricity.


    Quote

    Just speculating here, but if polonium-210 production could be carried out on Mars you could make the trip to Mars in a few months or less and then obviously swap out the little power source for the return trip.

    Swap it out? With what? Another PO-210 based RTG? Won't work. Polonium 210 is highly radioactive. The polonium doesn't care if the generated heat is put to productive use or is just radiated out into space.
  4. In Topic: Are there habitable planets/moons in our solar system?

    26 April 2012 - 11:15 PM

    Yes, there is at least one habitable planet or moon in our solar system.
  5. In Topic: Trying to integrate a function

    26 April 2012 - 05:04 PM

    View PostTheLivingMartyr, on 26 April 2012 - 03:17 PM, said:

    Well, the aim of this post was to learn something about integration, I now realise why this function can't be integrated to another function, because this function clearly isn't a product, and no substitution will leave you with du as a scaled form of dx. Sorry for the basic terminology, but I understand why it can't be integrated now!

    The problem is not that this integral doesn't exist. It most certainly does exist. The problem is that this integral can't be expressed in terms of the elementary functions. All the neat tricks that you have learned are aimed at solving those integrals than can be expressed in terms of elementary functions.

    Most integrals cannot be expressed that way. For example, students regularly ask how to integrate \exp(x^2) or \exp(-x^2). Play around with u-substitutions, integration by parts, etc., and no matter what you do you will either get an intractable mess or just get right back to square one.

    That doesn't mean the integral doesn't exist. It does exist. It turns out that f(x) = \frac{\,2}{\surd\pi}\int_0^x \exp(-t^2)\,dt is a very important function. It appears so often, and in so many different settings, that it has been given a special name (the error function) and a special symbol \textrm{erf}(x). The error function is just one of many integrals that can't be expressed in terms of elementary functions and that rear their ugly heads over and over again. These "special functions" will be the subject of multiple advanced math classes should you go that far in math.

    Quote

    Now, although I'm perfectly aware I'm probably getting ahead of myself, what is this "Elliptic Integral" supposed to achieve?

    Amongst other things, the arc length along a segment of an ellipse. Elliptical integrals are one of those things that keep coming up again, and hence they are given a special name.

Comments

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  1. Photo

    Cap'n Refsmmat 

    12 Nov 2010 - 23:43
    Hey, if you could let me know if you hit that weird HTML problem when making a post, that'd be great. I just upgraded to the latest version of the forum software and I'll have to file a bug report if the issue's still there.
  2. Photo

    mrsamer 

    22 Sep 2009 - 11:54
    Hi, i guess there is a spam post in my thread: [url]http://www.scienceforums.net/forum/showthread.php?p=516119#post516119[/url] thx
  3. Photo

    dr.syntax 

    04 Sep 2009 - 01:46
    DH, Thank you for sparing me anymore embarrasment. I deleted that Snell`s law posting as best I could. ...Dr.Syntax
  4. Photo

    Vindhya 

    18 Mar 2009 - 16:25
    Thank you very much sir.
  5. Photo

    Gravityforce 

    05 Jan 2009 - 22:56
    DH. I am sorry to you for any rude comments a directed at you. I know I don't deserve and help from you, but if you have the capability, could you help me remove the post and corresponding threads. Once again I am sorry
  6. Photo

    MolecularEnergy 

    21 Dec 2008 - 01:41
    DH, i am sorry also. I never meant to act like a real ****.
  7. Photo

    snp.gupta 

    18 Dec 2008 - 23:44
    Great sir
  8. Photo

    freezy 

    19 Jun 2008 - 19:17
    Pyro? edit: Sorry, I mistook you for someone else.
  9. Photo

    ydoaPs 

    13 Jun 2008 - 00:54
    Congrats on making expert!
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