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#51 Re: Human missions » Marsdrive Mission Design » 2007-09-08 06:26:49

You rescue them by sending them a replacement habitat... in the form of the first cargo delivery vehicle (as mentioned).

Attempting to bring them back home would be way more risky. Actually, if the hab became unhabitable either in transit or on the surface, both the Mars Direct and Design Reference Mission plans would be no better.

This plan is bulletproof.

I will now unceremoniously offer it to the Marsdrive people as a gift.

Use it wisely.

#52 Re: Human missions » Marsdrive Mission Design » 2007-09-08 06:15:57

The plan is more cunning than I originally thought. Think about it: It will be the new ISS. But without the shear pointlessness:

At first it will be a political solution to maintain the NASA army, then once the first crew is sent, it will become politically unkillable.

Pure genious!

#53 Re: Human missions » Marsdrive Mission Design » 2007-09-08 06:07:01

Before anyone says sustaining the crew isn't cheap: What I mean is, there is no big development costs required. Just an extra launch required every now and then to sustain the crew.

It's a strategy that would make everyone happy really. I imagine it could be a natural continuation of the Apollo Redux. Then, as now and before, NASA will want to find ways to justify keeping their workforce employed. Congress won't want to give out any extra cash. Its a sustainable solution that fits better with the new NASA philosophy.

#54 Re: Terraformation » Terraforming Venus - The Latest Thinking » 2007-09-08 05:52:52

Would it be possible to drive off some CO2 by adding more heat?

This may seem counterintuitive, but I'd be interested to know what effects heating Venus' atmosphere may have.

#55 Re: Human missions » Marsdrive Mission Design » 2007-09-08 00:12:33

Here's my suggestion (I thought of it while in the shower an hour ago in response to your post):

Radical Manned Mars Mission Architecture:

- Utilizing the Ares V SDLV and Orion derived Hab architecture. It is a direct continuation of Project Constellation.

- Under the plan, an ERV, together with the required in-situ technology and large nuclear power source, is not initially required, if at all. This enables the mission to be executed immediately after the new Lunar goals have been fulfilled.

- Initially, a Hab module is all that is required. This will be smaller than the Mars Direct hab, with a crew of 3, but will contain vastly more consumables.

- After the crew safely lands on the surface, the goal becomes increasing the crews tenure and ability to perform useful science.

- To meet these goals, succesive deliveries are of cargo vehicles, which contain more consumables, spare parts, scientific equipment, etc.

- These cargo vehicles are based directly on the Hab architecture, and may even provide a substitute living space in case of primary hab failure; thus further improving crew survivability.

- One particularly important piece of cargo may be a wheeled truss assembly, together with a small RTG power source, both of which can be easily bolted to the frame of the Hab to make it mobile.

- Having a mobile hab greatly increases science return, and at the same time improves crew morale. I beleive it is also a much safer alternative to long-range rover sorties.

- The 'initially one-way' mission architecture is politically unkillable, and also much more sustainable under NASA's new fixed budget.

- This means surface operations can be gradually expanded as more crews are sent, along with the successive cargo vehicles required to sustain them.

- Over time, the technology required to bring the crews back home may eventually develop. In fact, the uniquely flexible 'initially one-way' architecture will not only ensure continuous funding over many years (in order to sustain the crews on the surface), but may also practically guarantee that the funding is made available in order to develop the technology required to bring them home safely.

- Perhaps the beauty of this plan then, is not in its cost savings, but in the way in which it practically guarantees funding. However, the plan would require vastly less initial development costs, and would therefore be very easy to implement.

- The other issue is that of asset building and science return. Previous mission architectures have simply discarded previous assets (science equipment, life support, energy supplies, etc.) on the surface. With this new architecture, assets are kept with crew for a much longer period.

- The number one asset is the crew themselves, and this is why the architecture should have way more bang-for-buck than previous architectures. By keeping the crew on the surface for longer, much more science can be accomplished, and there is the benefit of building on previous knowledge.

- The crew will have the best science equipment available to them in succesive cargo missions. This means that samples are not needed to be returned to Earth for analysis. All the necessary data will simply be beamed back to Earth.


Summing it up:

* Sending the crew is relatively cheap and easy.

* Sustaining the crew is relatively cheap and easy.

* Getting them back safely is the difficult and expensive bit.

* But once they're there, no politician would dare condemn them to the surface. Funding would be guaranteed.

#56 Re: Interplanetary transportation » The solution of all Ares-I problems: the "J-2Y" engine >>> » 2007-09-07 22:35:50

Gaetanomarano brings up an interesting point about the potential to simply resize the engine for more thrust...

Obviously, for engines already in production, the cost would be significant due to retooling. But, as far as I know, production of the new J2 engine hasn't yet started, so I think he has a valid point.

#57 Re: Interplanetary transportation » Ares V (CaLV) - status » 2007-09-07 22:12:25

Hang on... Has there been an official policy change to reflect this?

Why is there an Orion on the Ares V?

#58 Re: Interplanetary transportation » Shipyards » 2007-08-29 01:18:11

Just out of curiosity, and I'm sure it has been discussed before; what is the cost of sending payloads to orbit in fuel costs alone (using current fuel prices)?

#59 Re: Interplanetary transportation » Really big rockets » 2007-08-29 00:57:30

Yeah, why not?

With current technology, how big can we go?

Is there a limit?

#60 Re: Terraformation » Mirror Array on Mercury? » 2007-08-23 01:21:52

Actually, yesterday I was reading about the effects of Libration (http://en.wikipedia.org/wiki/Libration), which makes the Terminator Zone (http://en.wikipedia.org/wiki/Terminator_%28solar%29) move around during the orbit of Mercury. This might make a Heat Engine (http://en.wikipedia.org/wiki/Heat_engine) on the surface difficult, but still possible. What I propose is some sort of fluid conduit between the hot and cold sides of Mercury, across the terminator zone, which transfers fluid energy to a generator. The advantage of locating such a heat engine on the surface of Mercury is that a huge heat-sink (the cold rocks on the dark side of Mercury) is available for conduction-based heat rejection. This is opposed to using radiation-based heat rejection available in the vacuum of space, which is extremely slow.

On a related, but somewhat macabre, note; I read somewhere that a human body, if ejected into the vacuum of space, would actually stay warm for hours (i.e. not instantly freeze to death). Rather, one would die of asphyxiation, independant of any other cause. Heat rejection via pure radiation is apparently very slow.

#61 Re: Terraformation » Mirror Array on Mercury? » 2007-08-22 03:08:33

Well, you could have two or more mirrors. One on Mercury to beam the concentrated light, and one in orbit, or held stationary by light pressure, around the planet itself. Maybe another one in orbit above mercury, or held by light pressure above the sun.

Here's another thought: Has anyone considered using the extreme temperature variation across the surface of Mercury to generate electricity?

#62 Re: Interplanetary transportation » Really big rockets » 2007-08-06 11:22:43

What about clustering simple solid rockets, or even hybrid rockets (like the one used in Burt Rutans SpaceShipOne)? Maybe something like OTRAG but with far bigger rockets, and in smaller clusters. Maybe reusable too.

Without considering the huge g-forces, how much payload could a cluster of 7 Shuttle SRB's lift? Consider a reasonably sized H2O2 upper stage, or perhaps even another SRB as the upper stage.

#63 Re: Interplanetary transportation » Really big rockets » 2007-08-05 22:45:16

Here's something on the russian RLA-150, the design predecessor to the Energia, from Astronautix:

http://www.astronautix.com/lvs/rla150.htm

rla150.jpg

The RLA cluster method would allow the modules to be built in the factory and thoroughly tested individually without risking the entire launch vehicle.

The modules had a gross mass of about 800 tonnes kgf each, were six metres in diameter and about thirty metres long.

The RLA-150 had a gross lift-off mass 6,000 tonnes, payload to low earth orbit 250 tonnes with six modules as the first stage, and the RLA-120 core.

Glushko insisted that a permanent lunar base and Mars expeditions in the 1980's were achievable. What was needed was a reliable heavy lift launch vehicle, and the RLA approach would achieve this.

The members of the VPK met the proposal with considerable scepticism. The final decision was that the plan had to be reworked. Brezhnev, Keldysh, and Ustinov would insist in the reformulation that the Lox/LH2 technology and capabilities of the US space shuttle had to be duplicated. The end result would be the Energia launch vehicle and Buran space shuttle, with which neither the military or the Soviet engineering community was happy.

I hate the shuttle.

#64 Re: Interplanetary transportation » Really big rockets » 2007-08-05 22:06:31

Alright, scratch the whole Paris launcher thingie... What would a clean-slate big dumb launcher look like?

#65 Re: Science, Technology, and Astronomy » The Clean-Slate City-State » 2007-08-05 05:17:47

Moreover, it doesn't really require these aforementioned apocalyptic scenarios to actually take place. I'm hoping international concern will be enough by itself. But there are other advantages too, which I shall cover further. I'll keep you posted.

#66 Re: Science, Technology, and Astronomy » The Clean-Slate City-State » 2007-08-05 00:30:36

Good questions.

"The Clean Slate Solution" (http://cleanslate.editboard.com/Discuss … on-t23.htm) should give you some answers.

But there are myriad advantages that a clean-slate city could have over established cities. I believe there are already a few clean-slate cities popping up in asia. But the fact that this will be a clean-slate government aswell puts it on another a level.

Why will Australia cede sovereign control of its territory to you? In particular, why will it give up its power to tax Clean Slate City?

That is a very good question. The reason they might do this is because 1. they have nothing to lose (its a desolate piece of land with no natural resources), and 2. they have a great deal to gain. That is, there will be economic benefit to Australia from the project. Perhaps I should cover this in more detail later...

Is Clean Slate City only possible if its inhabitants are wealthy?

In your mind, what are the main problems caused by including poor people?

I can imagine that the city will be seen as an attractive and desirable place to live. Hopefully, if demand outstrips supply, high premiums will be paid to reserve a spot in the city. However, as the city grows, the economy will diversify. And to ensure international competitiveness (in the manufacturing industry for example) then there would have to be people willing to work for low wages. So yeah, you'd eventually allow a lower class to migrate to the city to support these industries. But I can imagine that even this lower class will be better off than most, what with the advantages of a good wellfare system, government employment system, etc.

#67 Re: Science, Technology, and Astronomy » The Clean-Slate City-State » 2007-08-04 23:37:02

I'm not sure how much emphasis I put in that particular text, but the number one rule of this clean-slate city-state should be that it is not idealistic. I think the dystopian painting at the top is throwing readers off...

But yeah, I think too much wishful thinking during planning has ruined clean-slate city projects of the past. To avoid that, this city should be designed in a way that it gives the illusion of development history and organic growth. Portions of it may attempt to replicate great historic meditierranean cities. Other parts may be like London or New York. Variety should be the number one mantra.

The other difference is that this city will be its own sovereign state; isolated from the rest of the country. I can imagine the initial demographic of immigrants will be something like that of Dubai, where at least initially, people will pay a premium to live and work in the city. People will come here because they want to, not because of need. It will not be a 'dumping ground for the poor'.

#68 Re: Science, Technology, and Astronomy » The Clean-Slate City-State » 2007-08-03 09:51:34

FYI, I've just added heaps more info to the site.

Check out the top three topics at http://cleanslate.editboard.com/Discuss … ics-f2.htm.

Tell me what you think.

#69 Re: Interplanetary transportation » Really big rockets » 2007-08-02 05:52:05

Okay, I really want to develop the PARIS concept further. Can anyone help me? Any suggestions? Reference material? Rocket performance calculators, etc?

#70 Re: Interplanetary transportation » Really big rockets » 2007-07-26 00:00:32

I'm voting for Barrack.

Hang on a mo... That 2.5%... is that the chance that one engine out of 49 will fail? That wouldn't be so bad; I reckon you could probably design the rocket to accomodate this sort of failure. Afterall, thats only a decrease of 1/49th of thrust, or roughly a 2% loss. The rocket could probably just burn for a little longer in compensation without incurring too much of a performance penalty. Furthermore, the remaining engines could just be throttled-up to 102% thrust each (or whatever is required to make up for the ~2% loss). No biggie. Unless you're talking catastrophic failure... but engine monitoring systems seem to be pretty good these days and should shut it down before it explodes...

#71 Re: Terraformation » Game on Colonization / Terraforming of Mars » 2007-07-18 22:39:35

Could you go into more detail about the base-building / colonization part of the game?

#73 Re: Terraformation » Mirror Array on Mercury? » 2007-06-17 00:52:41

I was readng the "Terraforming Jupiter's Moons" thread when I came across noosfractals suggestion of using a smaller fresnel lens close to the sun to beam concentrated light to the moons of jupiter (to aid their habitability), instead of using a larger concentrator closer to the moon itself.

This made me think of using a mirror array (made up of many individually movable mirrors) on the surface of Mercury to achieve the same job. Of course, they will have to withstand those high surface temperatures, but this idea has the advantage that the mirror array can be constructed and supported on the surface and built from local materials. Perhaps each segment can be built on the cold side and transported around to the hot side when completed.

Has this idea been proposed before?

#74 Re: Science, Technology, and Astronomy » Mercury Mirror Space Telescope » 2007-06-15 14:27:02

Thanks Bob (can I call you Bob?). I wonder about liquid mirror space telescopes which don't use artificial gravity, but instead rely on surface tension or pressure effects. Do you know of any other sources of information besides the book and the sci.astro thread?

Was there any further discussion after that sci.astro thread?

#75 Re: Science, Technology, and Astronomy » Mercury Mirror Space Telescope » 2007-06-15 00:30:52

Here's another idea I just thought of. Remember when I suggested that accelerating a terrestrial mercury mirror telescope horizontally would allow the telescope to be tilted briefly? That idea probably wouldn't work very well on earth, because the gravity is very high. For example, if I wanted to tilt my mercury telescope 45-degrees, it would require a horizontal acceleration of 1g to be sustained for as long as the required exposure time. Its obvious that that wouldn't work if the exposure time is anything more than a few tenths of second.

However, for a mercury mirror telescope situated on the moon, the horizontal acceleration required to tilt the telescope at 45-degrees is the same as the moons gravity (1.62 m/s2 instead of 9.81 m/s^2). This might be reduced enough to allow this method to be useful. Perhaps the telescope can be situated on an even lighter body, such as an asteroid.

Another thought is that a hybrid thrust-induced and rotation-induced acceleration system may be possible (i.e. using rocket thrust to allow a tether-based mercury mirror space telescope to point at an angle in a similar way to the system described above). Because a tethered mercury mirror telescope only induces a tiny centripetal force, only an equivalently tiny horizontal acceleration would be needed for it to tilt at an angle. The ability to tilt could also be used to reduce the effects of motion blur.

Sloshing effects might be a problem though...

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