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#6351 Re: Human missions » International Space Station (ISS / Alpha) » 2012-07-02 13:12:39

Excuse me, I remain a sceptic. I recall the graph showing just how much of the NASA budget was being gobbled up by the ISS (in addition to the Space Shuttle that is).   For all that investment we could have set shop on Moon and Mars and visited Ceres and Titan as well.

#6352 Re: Terraformation » Titan, with modest efforts » 2012-07-02 12:14:01

Titan has a pretty strong romantic appeal for me. Probably, after Mars, it is the one Spheb (I just made that up - spherical body) I would like us to visit in the solar system. 

What a shame it was that the NASA guy pulled the wrong switch and we got so few photos...but what we got was amazing and intriguing.

I would hope we develop all sorts of robots to investigate the planet, especially with a view to seeing if we can find alternative life forms there.  A multi-abled craft - something that could roam, float, dive and fly would be good!

#6353 Re: Interplanetary transportation » Paraffin, propulsion and other uses, crash-landing it. » 2012-07-01 10:55:16

Void wrote:

I was at the www.space.com site to find this which I liked, and then did some related searching and thinking:

http://www.space.com/16378-hybrid-rocke … t-spg.html

Quote:

A new hybrid rocket motor fired up Friday (June 29), demonstrating technology that its builders say could lead to efficient, alternative-fuel launch vehicles down the road.

California-based Space Propulsion Group, Inc. (SPG) test-fired the 22-inch-wide (56-centimeter) liquid oxygen/paraffin motor for about 20 seconds Friday, blasting a streak of bright flame into the air at the company's testing facility in Butte, Mont.

The trial was the fifth for this particular motor, SPG officials said, and it demonstrated a flight-weight version of the design.



The company says future propulsion systems using the motor's hybrid technology have the potential to be five to 10 times cheaper than existing rockets. And the paraffin fuel has the added benefit of being non-toxic, officials said.

"We believe propulsion drives the cost of access to space and that complexity generally drives propulsion system cost," SPG president and chief technical officer Arif Karabeyoglu said in a statement after the test-fire. "By using a commercially available paraffin-based fuel, we have created an economically viable alternative that could significantly reduce the price of space accessibility, as well as help preserve the environment."

Hybrid rocket motors use propellants that are in two different states of matter, as opposed to purely liquid or solid rockets.

Proponents of hybrid technology claim that it combines the advantages of the other two types, offering the simplicity of solid systems and the safety of liquid rockets. (Solid rockets, such as the boosters that helped loft NASA's now-retired space shuttle, generally can't be shut off once they've been lit.)

Hybrid rockets are playing a large role in the burgeoning private spaceflight industry. Virgin Galactic's suborbital SpaceShipTwo vehicle employs hybrid motors, as does Sierra Nevada's Dream Chaser, a mini-shuttle that's in the running to transport NASA astronauts to and from the International Space Station.

Follow SPACE.com on Twitter @Spacedotcom. We're also on Facebook and Google+.

Quote Again specifically:

The company says future propulsion systems using the motor's hybrid technology have the potential to be five to 10 times cheaper than existing rockets. And the paraffin fuel has the added benefit of being non-toxic, officials said.



Paraffin
http://en.wikipedia.org/wiki/Paraffin

http://upload.wikimedia.org/wikipedia/c … raffin.jpg

Quote:

Paraffin waxParaffin wax (or simply "paraffin", but see alternative name for kerosene, above) is mostly found as a white, odorless, tasteless, waxy solid, with a typical melting point between about 46 and 68 °C (115 and 154 °F),[4] and having a density of around 0.9 g/cm3.[5] It is insoluble in water, but soluble in ether, benzene, and certain esters. Paraffin is unaffected by most common chemical reagents but burns readily.[6]

Pure paraffin wax is an excellent electrical insulator, with an electrical resistivity of between 1013 and 1017 ohm metre.[7] This is better than nearly all other materials except some plastics (notably Teflon). It is an effective neutron moderator and was used in James Chadwick's 1932 experiments to identify the neutron.[8][9]

Paraffin wax is an excellent material to store heat, having a specific heat capacity of 2.14–2.9 J g−1 K−1 (joule per gram kelvin) and a heat of fusion of 200–220 J g−1.[10] This property is exploited in modified drywall for home building material: a certain type (with the right melting point) of wax is infused in the drywall during manufacture so that, when installed, it melts during the day, absorbing heat, and solidifies again at night, releasing the heat.[11] Paraffin wax phase change cooling coupled with retractable radiators was used to cool the electronics of the Lunar Rover.[12] Wax expands considerably when it melts and this allows its use in wax thermostatic element thermostats for industrial, domestic and, particularly, automobile purposes.[13][14]

In industrial applications, it is often useful to modify the crystal properties of the paraffin wax, typically by adding branching to the existing carbon backbone chain. The modification is usually done with additives, such as EVA copolymers, microcrystalline wax, or forms of polyethylene. The branched properties result in a modified paraffin with a higher viscosity, smaller crystalline structure, and modified functional properties. Pure paraffin wax is rarely used for carving original models for casting metal and other materials in the lost wax process, as it is relatively brittle at room temperature and presents the risks of chipping and breakage when worked. Soft and pliable waxes, like beeswax, may be preferred for such sculpture, but "investment casting waxes," often paraffin-based, are expressly formulated for the purpose

So, I can see making old fashoioned "Potted" electircal devices if necessary.  (You never know what emergency might happen)

Or using the stuff to maintain comfortable/habitible conditions in a habitat, per temperature regulation.  It apparently was already used on the Moon for a cooling fluid, how about a heating fluid on Mars?

As a Rocket fuel.

TwinBeam mentioned crash-landing raw materials on another thread, I mentioned a "chain method" also on that thread, but it has other traffic of another nature, and this would step on that so I am starting this thread.

It seems to me that it would be a good candidate for hard landing/crash landing.

If packets of it were strapped on to the sides of a lander, and the lander had a spin at the time of release, the the bags of paraffin would eject from the lander and reduce it's load.  If there were air/Nitrogen bubbles in the plastic phase paraffin, then upon impact, the air bubbles would absorb some of the shock, and perhaps keep the bags from bursting.  Even if they burst, I am inclinded to think that the paraffin would largely be usible for a reasonable period of time, with cleaning.

I am wondering if instead of bringing Hydrogen to Mars, and extracting Oxygen from the atmosphere from it, it would be better to use paraffin as the fuel, and then simply extract Oxygen from CO2 directly, and casting away the CO remnant?

Hydrogen would be hard to deliver to Mars as a liquid.  Water would be expensive to deliver to Mars, since you are delivering a lot of Oxygen.

If Parafin can be eject-landed, and Oxygen pulled directly from the CO2, then the humans would simply pick up the solid pieces of bagged paraffin, and use it during the mission for what utility it had, and the reuse it as a fuel to get to orbit.









The following is not part of this topic, but it is interesting.  Maybe later:
http://www.space.com/16367-private-moon … almaz.html


Interesting - I do favour the "rough landing" as I would call it of "non-delicates".  However, I see no reason to add to the mass burden if we can use ISRU.  I really don't think heating habitats will be a problem if we land lightweight PV panels.   Burning paraffin on a constant basis would require monitoring.

There may be some argument for landing it on the first mission if we want to be sure of a return fuel supply I guess.

#6354 Re: Unmanned probes » Weather reports for Mars » 2012-06-29 13:29:49

In case any newbies aren't aware of this site:

http://www.msss.com/msss_images/latest_weather.html

It's great for Mars weather and latest views of the planet.

#6355 Re: Planetary transportation » Trains on Mars - Could a rail system provide martian need » 2012-06-28 15:36:33

Trebuchet wrote:

Actually, I think rail gets built fairly early on Mars - at least just around the main base to start. Some other thoughts...

Railroads, I think, would mostly be a problem because of steel consumption. Construction of a railroad would actually be cheaper and faster per mile, in terms of work, than on Earth.

* You don't need traditional ballast, at least until you start warming Mars up. Just use water - the ice would be fantastically hard and strong under Mars conditions, and you could melt the top to a very fine level. Sink the concrete ties in it and attach the rails

* in the low gravity, bridging and viaducts would be simpler to build than on Earth, as well.

* Steel wheels are easier than rubber wheels on Mars.

An option which might be profitably discussed would be an ice plateway - a flattened ice road with two grooves for steel wheels, rather than two rails. While this would have severe issues in terms of maximum speed, we're not terribly concerned with maximum speed, are we? And such roads would be fairly inexpensive to build, and could be upgraded to rail as steel production allowed.

Why do people build railways on Earth? Because (a) they need to move thousands upon thousands of tonnes to serve millions of people (b) because the terrain - with bogs, and rivers, mountains and so on, are not well suited to roads and road traffic and (c) because rail can go faster than road.

Neither of those drivers will apply on Mars in the early decades. (a)  The early communities will only need a few tonnes of this and that per month (b) the terrain - certainly in the areas where we will site the first bases - will be firm and well suited to road traffic once the rocks and boulders are removed and (c) we won't have the technology in place to build bullet trains on Mars - the gain in speed will be minimal, possibly non-existent.

Incidentally,we can use steel wire wheels on Mars.

#6356 Re: Science, Technology, and Astronomy » Nuclear airliners » 2012-06-26 15:58:13

RobertDyck wrote:

Chemical rockets are roughly 1% payload. Even with LH2/LOX, which has a much higher Isp than methane. You'll never get an SSTO or any truely cost effective reusable shuttle using chemical rockets.

But I started this discussion with airliners. Oil is way too expensive, and will only get more so. Kerosene based jet fuel, or any substitute that uses oil based fuel to make it, will also increase.

I started this by asking if you are ready to accept a nuclear airliner. I guess the answer is no. That means you will experience ever increasing air fare, and a dramatic jump when the US federal government no longer pays for airports.


There are more realistic alternatives than dangerous nuclear power:

http://www.guardian.co.uk/environment/2 … green-fuel

#6358 Interplanetary transportation » Mystery of the deep - a UFO? » 2012-06-26 12:28:18

louis
Replies: 1

I don't suppose it will end up being one, but this must be one of the best UFO stories of recent years:

http://www.dailymail.co.uk/sciencetech/ … -200m.html

Any thoughts?

#6359 Re: Science, Technology, and Astronomy » Nuclear airliners » 2012-06-26 02:17:07

Glandu wrote:
louis wrote:

Rail doesn't take you to your door. A car does. So does a bike.   I wonder if the survey included the energy expenditure of getting to the rail station and hanging around waiting for trains?

Nope : it's energy per pessenger per kilometer(forgot the unit, just remembers the scale). With streetcars(i.e. american-style small scale tramways), though, you can go rather near home. If we don't find adequate replacement to petrol, public transit will have its importance improved - and cities will need to be more dense, more Washington DC than Calgary. Note though that for cities with heavy slopes, tyres are still useful - that's why inhabitants of San Francisco avoid the cable car & use trollebuses instead. Only tourists use cable car.

Nuclear planes might be useful for transatlantic transport, but won't for going from home to work.

Of one thing I'm sure, we already have the answer to petrol for cars.

Utah University has already built electric roads which could be used to power electric vehicles through wireless charging. And of course the electricity for the vehicles can come from wind and solar (plus hydro, energy from waste etc) any time.  Toyota has developed a new highly efficient battery which should be out in the next year or so which is a bit of a game changer - extending range at lower cost, which will also help greatly. The primary roads can have the wireless electric charging - for the rest of our journeys we can rely on the batteries which we either charging at home or whileon the primary roads.

#6360 Re: Human missions » Landing on Mars » 2012-06-25 17:34:25

GW Johnson wrote:

ISRU cement is an unknown for a while yet.  There's some ideas floating around,  but cement as we know it here won't set there:  too cold.  "Icecrete" is one candidate,  but you have to protect it from sublimation by a coating or by burial,  and you have to insulate heavily to keep it from melting. 

There's an underwater habitat-of-sorts idea floating around,  too.  In places on Mars where there is a buried glacier,  you can just melt out a huge pond,  and cover it with re-frozen pack ice and a regolith cover over that.  If the pack ice is thick enough,  the pressure in the water underneath may be high enough to support life in a wet suit and SCUBA,  not a pressure suit.  Takes about 6-7 meters of ice,  I think. 

In the pond,  use lights to support photosynthesis in an aquaculture environment,  and the waste heat from the lights keeps the pond from refreezing.  There's no pressure dome;  this could cover acres and acres,  as big as desired.  You import organic matter and organisms,  and grow water plants and animals.  Some could be fresh,  others saline. 

You could do this same under-ice thing in the trench you suggested,  Louis.  You just need a sealant of some kind to keep the liquid water from sinking into the subsurface geology. 

GW


Yes, that's an interesting idea - creating large areas of aquaculture...

While we are on the subject of large spaces, you could throw in my small canyon idea - find a a narrow canyon over which you can put in a roof. Maybe bulldoze and compact material at either end. You could, very cheaply have a large living space that could be pressurised and in which you could create a kind of biosphere (though with venting and inputs).

On the cement, I was thinking of this as a smooth lining for the interior of the trench.  I have always imagined you would have some sort of low pressure work tent over and keep the space at a desired temperature, so I would hope cold would not be an issue in itself.

#6361 Re: Science, Technology, and Astronomy » Nuclear airliners » 2012-06-25 14:56:36

Glandu wrote:
GW Johnson wrote:

All that I said in post no. 18 being what it is,  I think the sense of Robert Dyck in post no. 1 is correct.  We need a cheaper way to fly,  one that is more or less independent of oil prices.  If that's some nuclear engine,  then so be it. 
(.../...)GW

IIRC, I read a french study about the 2000-2009 decade, summarizing the energy consuption of different transport modes per pessenger. It was like :

_Rail : 0.2
_Boat : 0.4
_Tyres : 2.2
_Air : 3.2

For anything not transoceanic, rail it the obvious choice. But Transatlantys is not for tomorrow(it was an advertisment joke promising a train tunnel between France & New York City).

I'm not sure coing nuclear would significantly reduce the energy cost of an airplane(in terms of joules, not in terms of $).

Rail doesn't take you to your door. A car does. So does a bike.   I wonder if the survey included the energy expenditure of getting to the rail station and hanging around waiting for trains?

#6362 Re: Human missions » Landing on Mars » 2012-06-25 13:40:20

GW Johnson wrote:

Here's a notion for a quick habitat using something similar to a Bigelow inflatable.  Have your equipment on a core structure to which the inflatable "shell" is already packaged around.  This core has hard ends where the legs are.  It sits on its side on those legs and inflates as an off-centered cylinder such that there is more volume above than below.  The airlocks are also on the ends.  You unpack your equipment inside,  just mount nothing on the inflatable wall.  Through something resembling an air mattress over it and inflate to not quite 7 mbar,  as insulation and a meteroid shield.  Throw an opaque tarp over that,  and stake it all down.  Voila:  instant inflatable habitat,  with all the gear already inside.  Land it as a pallet and just set it up like a giant tent.  There's probably a vertical-axis version,  but stairs would be less convenient inside. 

GW

Sounds good to me. It's remarkable that NASA has had so long to think about this sort of thing and not come up with anything specific.

My fave for creating habitat once there: dig a trench with the (1500 kg) mini digger you bring with you. Plaster the floor and sides with ISRU cement. Maybe embed air pipes for heating. Then place the steel sheets you have manufactured on Mars over the trench. Cover with a couple of metres of regolith. 

Could be very good for creating farm hab space.

Not sure how we deal with the air lock problem but I like the idea of using water to create an ice barrier externally. When you want to exit you melt the ice and the water drains away. After entry you freeze the water again (partly by exposure to the Mars atmosphere). 

Would require a lot of energy perhaps, but that is something we should have plenty of.

I think it's worth looking into - we need a simpler way of air locking than importing huge steel doors or attempting to manufacture them on Mars.

#6363 Re: Human missions » Landing on Mars » 2012-06-23 16:50:28

SpaceNut wrote:
RobS wrote:

I like the "log cabin" idea! But all the experts seem to think it's better to send one lander than four, probably because of the multiplier of expense, extra fuel, and more that can go wrong (nonfatally, that is). That's a lot of carbon dioxide filters to replace and other basic maintenance to do. When ISS had a crew of 3, two of them were busy with maintenance.

Since we know that we are not able to deliver the large tonnage to the surface that is needed so why not make it smaller packaged so that we can do what we will need.

Sometimes the simplest is the truest.

I don't know why people persist in planning to land large tonnages in one go , when you can get the tonnage you need to the surface in multiple missions.

#6364 Re: Interplanetary transportation » Airship to Orbit? » 2012-06-23 09:08:15

Void wrote:

I looked it over now, rather entertaining if nothing else.

http://en.wikipedia.org/wiki/Orbital_airship

http://www.jpaerospace.com/atohandout.pdf

http://www.jpaerospace.com/

http://en.wikipedia.org/wiki/JP_Aerospace#Ascender

The PDF is nice to look at.

I guess the part I like the best is where if they do have the "Dark Sky Stations" at 140,000 feet then Oxygen could be collected to fuel the Orbital assender.

I wonder if those stations could also make a buck being communication relays, and also hotels?  That might justify the stations and the ground to station airship.
The orbital assender is really outside of the box though.

I have plenty of reservations about how it could work, but I have thought of a few possible solutions for some problems.

I guess for the issue where space objects might puncture the orbital assender, I would speculate on small robots inside with patch kits, perhaps they would have Gecko feet to stick to the inside walls?

http://geckolab.lclark.edu/dept/geckostory.html

http://www.dailymail.co.uk/sciencetech/ … -mark.html


I am not sure but I am speculating that the "Electric" propulsion for the orbital assender might be a process of compressing electrostatically charged gas and venting it?

If the propulsion were electric, I would think that a powersat in orbit might be able to beam energy to it.  If it were microwave, however I guess I don't know how the airship could convert that to electricity.  If it were laser, and the skin was solar cells of a very thin type, then perhaps that could work.

I guess some time ago there was talk about super strong Nano Materials in the future.  Perhaps that would be required, to make a very thin but strong structure.

It is entertaining however far off it is to our current grasp.  I am glad that people are thinking so way far out.


Couldn't the DSS be a solar power station with thin PV film which then separates out oxygen to use as fuel?

I remember looking into JP a few years back and someone here did as it were "shoot them down in flames". They seem a lot more credible now. At least they're busy! And I like the way they mix the show business with the tech side of things. It's important if space commerce is going to take off.

I would be v. concern about puncturing of what appears as v. flimsy material, but I guess it might be OK for cargo, as you could carry that risk.

#6365 Re: Interplanetary transportation » Airship to Orbit? » 2012-06-23 08:55:40

Void wrote:

I looked it over now, rather entertaining if nothing else.

http://en.wikipedia.org/wiki/Orbital_airship

http://www.jpaerospace.com/atohandout.pdf

http://www.jpaerospace.com/

http://en.wikipedia.org/wiki/JP_Aerospace#Ascender

The PDF is nice to look at.

I guess the part I like the best is where if they do have the "Dark Sky Stations" at 140,000 feet then Oxygen could be collected to fuel the Orbital assender.

I wonder if those stations could also make a buck being communication relays, and also hotels?  That might justify the stations and the ground to station airship.
The orbital assender is really outside of the box though.

I have plenty of reservations about how it could work, but I have thought of a few possible solutions for some problems.

I guess for the issue where space objects might puncture the orbital assender, I would speculate on small robots inside with patch kits, perhaps they would have Gecko feet to stick to the inside walls?

http://geckolab.lclark.edu/dept/geckostory.html

http://www.dailymail.co.uk/sciencetech/ … -mark.html


I am not sure but I am speculating that the "Electric" propulsion for the orbital assender might be a process of compressing electrostatically charged gas and venting it?

If the propulsion were electric, I would think that a powersat in orbit might be able to beam energy to it.  If it were microwave, however I guess I don't know how the airship could convert that to electricity.  If it were laser, and the skin was solar cells of a very thin type, then perhaps that could work.

I guess some time ago there was talk about super strong Nano Materials in the future.  Perhaps that would be required, to make a very thin but strong structure.

It is entertaining however far off it is to our current grasp.  I am glad that people are thinking so way far out.

How about magnetic antennae to attract any stray bits of metal.

#6366 Re: Human missions » Landing on Mars » 2012-06-22 07:00:47

RobS wrote:

I like the "log cabin" idea! But all the experts seem to think it's better to send one lander than four, probably because of the multiplier of expense, extra fuel, and more that can go wrong (nonfatally, that is). That's a lot of carbon dioxide filters to replace and other basic maintenance to do. When ISS had a crew of 3, two of them were busy with maintenance.

But most experts call for (a) larger tonnages than are necessary and (b) ignore the ability to pre-land supplies robotically (as we land Rovers now).

The ISS is a complete hotch-potch of a thing...designed piecemeal.  I never use it as much of a guide to anything.  Two people, from a three man crew, got to the Moon no problem.  By the end I think the mission time was something like three weeks. That was 40 years ago.  I'd start there.

#6367 Re: Science, Technology, and Astronomy » Nuclear airliners » 2012-06-22 02:03:35

RobertDyck wrote:

So you guys want to go green. That's another discussion. Yes, I believe in green technology, and could list what I want to build into a house. However, none are practical for an airplane.

Ships cannot use wave power, they float so wave power is not compatible. The most efficient means of using wind to move a ship is sail, and wind turbines are not compatible with sail. So for a ship that leaves a combination of sail and solar. You could use photovoltaic for electric power generation, and sail to move the ship. Tall sailing ships do not move as fast as deisel, and the ship is at the mercy of weather (wind).

Wave power for use by sea vessels is certainly feasible. See this article:


http://inhabitat.com/transportation-tue … ered-boat/

I don't think we are talking about tall sailing ships - more likely fixed sails that extend either side of the ship AND aerial sails (like paragliding parachutes).  Both have been trialled.

Speculatively, one might also run out a huge solar PV surface on floats behind the ship (almost like a trawler net) that would generate huge amounts of PV electricity.

Obviously none of this is cost effective yet, but I think it could be in the same way wind turbines are now cost-effective over a period of 5-7 years. Toyota announced last year they had developed a new cheap battery that is about 5 times more efficient than current lithium batteries. That could make a huge difference.

As for aircraft, the most obvious power source is green bio fuels. Virgin Atlantic are already moving over to green bio  fuels. Longer term I think cold fusion may have the right mix of cost-effective power and energy density, but we await developments on that front.

#6368 Re: Human missions » Lunar Tourism is Go! » 2012-06-21 15:46:52

They do seem to have bought the space stations and imported them to the Isle of Man.

http://www.excaliburalmaz.com/0401_Press.html

#6369 Re: Human missions » Lunar Tourism is Go! » 2012-06-21 13:02:34

Terraformer wrote:

It was a Lunar flyby. That means you go around the moon, and yes, see the Lunar farside. This is in the same league, but almost twice as expensive, with a company that has no experience.

OK, I wasn't aware it was lunar flyby. Thanks for the info.

Personally I feel lunar tourism should wait until they can get people to the surface to stay in a hotel. That will increase demand tremendously I think.

#6370 Re: Human missions » Landing on Mars » 2012-06-21 06:18:04

Impaler wrote:

Splitting up the Crew while seemingly an attractive solution to the current mass limitations on EDL it is a huge multiplier for lose of crew and mission.  Also the surface habitat will almost certainly need to be monolithic or very near that and it's mass is going to drive the EDL tech, if we can't land a suitable habitat then theirs no mission even if Scotty could 'beam' them down.  Once we possess the EDL tech for the habitat, the crew is a rounding error.

As for trying to thrust upwards to slow-down laterally, I get your general drift but it seems to me that kind of flight-path would be best achieved by having a lifting shape and/or angle of entry so aerodynamics are converting that forward speed into gravity counteracting lift.  As crazy as it might sound perhaps we should examine something like the delta winged configuration.  A delta-wing vehicle can be placed nose-up or side-mount on a launch vehicle allowing a vastly larger heat-shield area vs round shields inside narrow payload fairings (Imagine how hard it would be to launch the shuttle if was put on the end of a rocket in the horizontal position).  Obliviously the lack of runways on Mars means a glider landing is out of the question so I'd just go to parachutes and rocket landing for the final descent (possibly detaching the whole delta-wing after it's no longer useful the way the heat-shield is typically dropped now). 

I don't have any idea what kind of peak heating such a shield would need to withstand, to be practical it would presumably need to be lower heating and lower weight then the shuttles system (can a launch-once, land-once system could do that).  Though when you consider that shuttle was able to bring down nearly as much cargo as it lifted (a capacity foolishly mandated and then virtually never used) and it was permanently stuck with the heavy engines in its rear (Unlike the Buran), plus a modest sized crew cabin.  All that together must add up to a considerable amount of potential down mass if it were all being used for payload. 

No idea if it would really work but the basic principle of putting the heat-shield in a vertical position during launch is the only way were ever going to get a ridged one of that size to Mars. If your not a fan of Delta-wing shapes a traditional conic shield might be launched in the same way.

Rune:  I think the Shuttle orbiter would be in the Beta range your looking for, I saw a figure of 376 m^2 for it's full profile but couldn't find the Ballistic coefficient it actually achieves on its entry angle-of-attack.  Maximum landing mass is 100 mt, well above what's needed so Beta could be brought down considerably by lightening the payload.  Also the total mass of thermal protection (belly, nose cone, leading edges, rudder cockpit all of it) is only 8500 kg, considerably less then I'd been lead to believe, naturally the tile system would be replaced with good-old ablative materials thus creating something vastly cheaper to build and probably lighter too.

I have always favoured crew splitting - two lots of 3 for me is best.  I think there are all sorts of advantages including an easier EDL task.

#6371 Re: Human missions » Lunar Tourism is Go! » 2012-06-21 06:15:49

Terraformer wrote:

Hmmm. Space Adventures have been offering the exact same experience for some time now, including a stay on the ISS, using a Soyuz capsule. Cheaper too, at 100 million dollars rather than pounds.

That they didn't get anyone taking up the offer says a lot about the market, doesn't it...

That wasn't for a trip to the dark side of the Moon was it?  This is in quite another league. I am not saying I find it credible, but I do find it interesting.

I think eventually we will see a link up between Space X and Virgin Galactic and trips to the Moon will be offered at far less than $100 million. Why not if launch costs to LEO are down to $2million per tonne?

#6372 Re: Human missions » Shenzhou 9 launch LIVE » 2012-06-20 18:16:25

JonClarke wrote:

You are assuming the only justification for the Chinese space progam is "glory".  The converse is true.  the Chinese space program is driven primarily about needing national needs, building capabilities they deem neccessary.  Hence the emphasis on Earth observation, communications, tracking and data relay, navigation, and technology development.  A crewed orbital laboratory is clear seen to be part of that.

Space exploration is a small part of this, but the Chang'e 1 and 2 missions have been grerat successes, Chang'e 2 is currently on the way to asteroid Toutatis for a January 2012 rendezvous.  More lunar and asteroid missions are under development.

They are in no hurry, there is no "race", they build capabilities rationally within the larger constraints of national policy.  They minimise risk, as any rational organisation does, with the result they have the most reliable rockets in large scale service today.  Space program goals are detailed in the five year plans, which to date have always been met, with longer term goals outlined to ten years out.

It is a very rational and admirable program.

You are talking about the regime that murders trade unionists and journalists, tortures nationalist protestors, was responsible for millions of deaths of its own citizens,  cheats at international trade, indulges in forced abortions, has the highest legal execution rate in teh world and zapped a satellite with a laser?

Please stop the Soviet-era propaganda. It's not at all "admirable" that a totalitarian regime should have a successful programme - it can only be worrying.

The Chinese with a population of one billion plus, all the resources of a centralised state since the Sputnik era - nearly five decades -  and the benefit of Soviet designs are not that impressive when compared to Space X who have managed to leap from nowhere to orbital assembly in 8 years. Let's hope they keep up their plodding progress.

#6373 Human missions » Lunar Tourism is Go! » 2012-06-20 17:30:53

louis
Replies: 5

Interesting article suggesting we might have lunar tourism earlier than many expect - by 2015! 

Actually I've no idea how credible this company (Excalibur) is. Does anyone else know much about them? They claim to be using ex-Russian craft.

http://www.dailymail.co.uk/travel/artic … -100m.html

But their plans certainly make me more confident that my prediction that lunar tourism would arrive sooner than expected could be correct. This is important for Mars simply, I believe, because it could generate such huge revenues - if Space X garners that revenue it will be put to good use in developing the human presence on Mars.

#6374 Re: Science, Technology, and Astronomy » Nuclear airliners » 2012-06-20 14:41:38

Terraformer wrote:

What about increasing the number of commercial nuclear ships? You could spin it as being more "green", reducing the "carbon emissions" fron shipping, while at the same time allowing cheap shipping to remain viable. We already know how to do nuclear with ships - a lot of navies do it regularly. Perhaps, with nuclear power plus drag reduction, we'll be able to increase the speed of the craft much more, so that it'll be a few days across the Atlantic.... Depending on the ticket price, that might be good enough for passengers...


What about green energy ships using a combination of solar power, wind turbine power, aerial sail  and wave power - all four have been trialled at sea and found feasible. Put the four energy sources together and you probably have a working system.

#6375 Re: Human missions » 50 years after... » 2012-06-20 02:18:55

Glandu wrote:

Nice quote, Louis, but the thing is we don't know yet how to land more than 2 tons on Mars. We have plans for landing more, but as long as it's just plans & noone does it, we don't really know how.

Landing on earth is not easy for us earthians, but we have a huge advantage over martians : we live here & know all the tricks. Americans did choose water landings because of their carrier fleet making recover easier & safer, USSR did choose desert landings due to lack of carriers & great number of appropriate deserts. Both of them did know & master the environment they did choose for the landings. Martians would not have that luxury. Their capsules would sink in the oceans, burn in the woods, be attacked in urban terran(by dogs or humans), sink in swamps.....

Once again, I believe we can land on Mars. Just, let's not assume it's easy. Politics means failure is not an option. and when you here this sentence, you know that your management has lost control of the situation.

I wasn't denying the reality of the problem! But how you feel about  a problem often determines whether you can resolve it.  It often does pay to look at problems from a different perspective.  It sometimes helps at work for instance when someone gets upset about an issue to ask them if this issue is going to make the headlines in the press the next day - given the answer is no, it immediately helps put things in perspective.  I think the thought experiment at least lets us realise that we are lucky in that in many ways Mars is a benign planet for human beings: better one third gravity than three times gravity! better carbon dioxide than sulphur dioxide etc. But I am not underestimating the difficulty of EDLA (we ought to add ascent to EDL)  to Mars.

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