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#5701 Re: Interplanetary transportation » Space X - If at first you don't succeed... » 2016-04-10 14:39:26

If a plane can fly 10,000 times, I think a first stage can fly 10 times, and maybe 100 times. Perfection takes some time to perfect but I think they are well on the way.

GW Johnson wrote:

Spacenut,  it's too early to hold them to such a standard.  Let them do it a few times,  and still fail some of them,  before you start judging.  By your standard,  we would have given up airplanes by the time of the Wright flyer crash that killed Lt. Selfridge.  Which was before WW1.  Not WW2;  the Great War,  WW1 !  1909 I think it was.
GW

#5702 Re: Interplanetary transportation » Space X - If at first you don't succeed... » 2016-04-08 16:10:59

Brilliant news! Congrats to everyone at Space X for this marvellous achievement. The era of cheap space travel beckons... smile Can lunar hotels be far behind?  I don't think so.

#5703 Re: Human missions » NASA: Mars colony may wait » 2016-04-05 13:49:00

I mentioned Space X.  I think it could be the lead participant. However, even Space X would, I think, struggle with developing an effective Mars-Earth coms network unless there have been technological changes I am unaware of. So that makes them dependent on NASA or some other big space agency. I think most long distance low power coms involves huge ground receivers.  Happy to be shown to be wrong on that!

Tom Kalbfus wrote:
louis wrote:

This is what happens when you have a lack of focus. If you have an organisation like NASA, where there are say 100 major projects,  they are all going to have their advocates whether it be robotics, another Titan lander, revisiting Pluto, lunar bases, weather forecasting, climate change monitoring, deep space exploration, solar panels, EM drive or whatever.  To  try and get a new major project in place is extremely difficult as you have to wade through a swamp of counter-advocacy and self-interest. What is required in my view is to create a new settlement-focussed agency - a Mars-Lunar Development Agency with the specific task of developing permanent human settlement on the Moon and Mars within 10-20 years. Ideally it would be an international agency that other democratic countries could buy into. On that basis, hiving off 20% of the NASA budget for the new agency should be enough.  The Agency would be more like an investor and so could then buy in services from agencies like NASA, Space X and so on.

Well there is SpaceX, doesn't that count? I think we have to put National Interests into space colonization and have competition, that is usually the best way to get things going. Once the UN Space treaty was signed, that took National Interest off the table, and we've had a directionless space program every since

#5704 Re: Human missions » NASA: Mars colony may wait » 2016-04-04 03:22:14

This is what happens when you have a lack of focus. If you have an organisation like NASA, where there are say 100 major projects,  they are all going to have their advocates whether it be robotics, another Titan lander, revisiting Pluto, lunar bases, weather forecasting, climate change monitoring, deep space exploration, solar panels, EM drive or whatever.  To  try and get a new major project in place is extremely difficult as you have to wade through a swamp of counter-advocacy and self-interest. What is required in my view is to create a new settlement-focussed agency - a Mars-Lunar Development Agency with the specific task of developing permanent human settlement on the Moon and Mars within 10-20 years. Ideally it would be an international agency that other democratic countries could buy into. On that basis, hiving off 20% of the NASA budget for the new agency should be enough.  The Agency would be more like an investor and so could then buy in services from agencies like NASA, Space X and so on.

#5706 Re: Martian Politics and Economy » Corporate Government » 2016-02-27 18:47:51

I think you actually need to explain what you mean...

"there are several corporations laying claim on Mars, and in fact in the proposed Act is a provision saying that no corporation (nor collection of corporations effectively under the same control) can have more than one claim, explicitly banning the monopolization of Mars."

That sounds v. much like the Antarctic Treaty where there are overlapping claims on territory. Only works as long as people keep their bases well separated.

My own view that it would be best if one (multi-agency) Mars Consortium took the lead in colonising Mars and thereafter established de facto supremacy.

IanM wrote:

I'm sure many of you have heard of the Space Settlement Institute, and their Space Settlement Prize Act: http://www.space-settlement-institute.o … e-act.html. Essentially, what it would do is have the US recognize claims made by a corporation up to a given area of land, in the case of Mars 3.6 million square miles for the first corporation to reach Mars and decreasing by 15% for each subsequent corporation reaching Mars. I sometimes daydream about being a surveyor on one of those claims, being the first ever human exploring given parts of the outback.

There are obviously some differences between that idea and yours, although both are examples of corporate governance:
-One of your key points is that there'd be one single corporation governing all of Mars. Here there are several corporations laying claim on Mars, and in fact in the proposed Act is a provision saying that no corporation (nor collection of corporations effectively under the same control) can have more than one claim, explicitly banning the monopolization of Mars.
-Your primary source of revenue would be in the transport and pre-homestead maintenance of settlers, while here the primary source of revenue is simply selling the land to the homesteaders.

Overall, I think your plan is better, but that is another way to think about corporations and Mars.

#5707 Re: Human missions » Mars Mission Comparisons - updated with kbd512's proposal » 2016-02-22 19:23:13

See below my response in bold...

SpaceNut wrote:

I found the other topic which is simular.... Index» Human missions» Mars Missions comparison

The list of attributes :
MISSION SIZE : What we do know is that crew size matter once we start to explore on the surface in that we would always want to explore in pairs.

I would agree. No one I know is arguing for solo exploration. Way too dangerous. 

PRE-MISSION CONTENT : If this is a preloading of a selected site that depends on mission length of time and crew size.

It's for people contributing to say what they envisage in the pre-mission period. Personally I think you need to cover (a) any pre landing of supplies/infrastructure (b) training and proving (c) establishing a (or utlising a pre-existing) Mars-Earth communication system.

LAUNCH : The big change in size is when we employ artificial gravity and preload mars landing site for how many launchers will be needed for the mission.

TRANSIT TO MARS : We know that chemical will give a 6 to 8 month travel and that cargo can go via ION propulsion much slower for non living transport. The chemical transit will depend on how large the ship is that we travel to mars in and that will impact the launcher count.

Isn't there also the option of a direct shot at Mars which is quicker (less than 6 months) but also more fuel-costly? 

++++++++ will finish thoughts later....

ENTRY, DESCENT AND LANDING/ASCENT AND RETURN :

ENERGY AND LIFE SUPPORT

MISSION CONTENT

COST/INCOME

#5708 Re: Human missions » Mars Mission Comparisons - updated with kbd512's proposal » 2016-02-22 19:15:35

I will try and incorporate that additional material as best as I can and then you can review. smile


kbd512 wrote:

One of my suggestions in another thread was sending two astronauts per DSH using two complete DSH's instead of one DSH.  It adds a measure of redundancy to the mission and a LOX/LH2 upper stage or stretch tank LOX/RP-1 could throw the DSH to TMI from LEO.  Each DSH is a single module that will fit inside the payload shroud of virtually any commodity heavy lift rocket.

Launch count is two Falcon Heavies to deliver two DSH's to LEO (and on to TMI after a Falcon 9 delivers the crews) and one Falcon 9 to deliver the crews.  Absolutely no orbital assembly is required for the DSH, no SEP-CTV is required to push the DSH to EML-1, you can obtain AG by tethering off to the upper stage, and your crewed vehicles are pushed through TMI from LEO using existing chemical propulsion technology.

We have to kill the structural mass of the DSH and upper stages using composite pressure vessels, but Boeing has proven that the things don't leak and weigh substantially less than aluminum.  If you want as near-term a solution as is practical, this is the solution.

The only SEP-CTV's absolutely required for the mission deliver the TEI kick stages and the MSH or MTVL's to Mars ahead of the crew.  The SEP-CTV's delivering the TEI kick stages would be responsible for mating the TEI kick stage to the DSH's for return to Earth and attitude control in LMO.

Edit: If an unpressurized two person capsule is used for the MDV and MAV, then the MDV can be mated to the DSH and delivered to Mars with the DSH, rather than requiring a Mars orbital rendezvous with the MDV.

An unpressurized two person MAV can be delivered to the surface of Mars of using Falcon Heavy and chemical propulsion.

So:

Window 1 ($500M in launch costs, about the same as 1 STS or 1 SLS flight):

* 2 Falcon Heavies deliver 2 MAV's to the surface of Mars using chemical propulsion and aerobraking

* 2 Falcon Heavies deliver 2 MSH's to the surface of Mars using chemical propulsion and aerobraking

Window 2 ($315M in launch costs, considerably less than 1 STS or 1 SLS flight):

* 2 Falcon Heavies deliver 2 DSH's with attached MDV's to LEO (integrated SEP still required to spiral in to LMO and to spiral in to L1)

* 1 Falcon 9 uses Dragon to transfer 4 crew to the 2 DSH's in LEO before TMI burn

No unaffordable super heavy lift rockets, unaffordable super heavy capsules, or SEP-CTV's are required for this mission architecture.  You can front load the mission with another two Falcon Heavies to add 2 more MSH's as second level surface backup or small pressurized rovers or throw heavier MSH's (by mating chemical kick stages to the MSH's in LEO).  However, we're well within the realm of science reality here and very comfortably within NASA's budget while still permitting us to maintain ISS and do other interesting things with NASA's budget.

End Edit

The MDV (Red Dragon), MAV (modified Red Dragon with larger LOX/LCH4 tanks), and even the MSH (if it's a reprise of Zubrin's combination MDV and MSH using a stowed inflatable) could be variations of the same piece of hardware.

That's the most affordable and practical human exploration of Mars mission structure that I can come up with.

International Participation Side Bar:

Each participating country would be required to purchase certified flight hardware (DSH, TMI/TEI kick stages, and SEP-CTV's; America would pick up the tab for the surface exploration hardware, MDV/MAV/MSH, and active radiation shielding hardware), provide their own launch services if desired, and staff a mission control facility.  We can afford to send 2 to 4 crew members per space-faring country.  Our maximum crew head count is 16 and I believe the scientific return would be far, far greater with 16 vs 4 crew members.  Mars Mission Control Center (MMCC) would rotate between Houston, Korolyov, Darmstadt, and Beijing in 6 hour shifts with a one-hour hand-off, so each facility only requires 8 hour staffing with an after-hours skeleton staff.

#5709 Re: Human missions » SLS and what asteriod will we go to » 2016-02-21 08:40:29

KIND OF OFF TOPIC:

Just to let you know kbd12 that I incorporated your mission outline in the Mars Missions comparison doc:

https://www.docdroid.net/vCwcfFY/mars-m … .docx.html


kbd512 wrote:
SpaceNut wrote:

Build it fly it is just a way to wring out the bugs as you have no set plans to build it from so you are doing R & D to develope the testing article for setting the steady state plans into motion to which you build the final manufactured item to.
The current level of ION thrusters are wimpy go look at my post in the SEP topic....for what we need versus what we have....

The only thing we need to do a Mars mission is a SEP-CTV and moderately sized chemical kick stages attached to SEP-CTV's.  If you accept the fact that not all missions have start in LEO, then you can do lots of exploration without enormous rockets.  LEO imposes a huge dV penalty that even the most evolved variant of SLS won't overcome.  The most powerful upper stage planned can throw just over 41t to TMI.  A $500M to $700M rocket is required just to throw 41t to TMI using chemical propellants.

If the SEP-CTV costs less than $250M, there's no economics argument on launch costs alone.  If SpaceX and ULA can reuse a booster just once and the price drops to $50M to $75M per launch, there's really no economics argument to be made.

If you mate a 30t-50t payload to a 30t-50t SEP-CTV using two Falcon Heavy or Vulcan rockets, you can throw the same payload for a fraction of the cost.  If you use commodity rockets from SpaceX and ULA, there's no $3B a year fixed program costs for NASA to pay to operate SLS and therefore plenty of money to purchase hardware and propellants for SEP-CTV's.

The SLS upper stage is a paper concept at this point.  Let's cut our losses and return to using moderately sized launch vehicles that have moderate operational costs so there's funding for payload development.  Now that SpaceX and ULA are competitors, both can bid on NASA contracts.  Both have the hardware and expertise to deliver payloads to LEO or GEO and that's all we really need them to do.

#5710 Human missions » Mars Mission Comparisons - updated with kbd512's proposal » 2016-02-19 19:25:49

louis
Replies: 17

I've updated my Mars Mission Comparison doc to include kbd512's "Affordable Human Exploration of Mars Program".


https://www.docdroid.net/vCwcfFY/mars-m … .docx.html

It's the no. 5 proposal -  to be found on page 8 of the doc.

If anyone would like to add another proposal (whether their own or some other agency), please just reply here with the text for each category under the first column in the table in the doc i.e.

MISSION SIZE

PRE-MISSION CONTENT

LAUNCH

TRANSIT TO MARS

ENTRY, DESCENT AND LANDING/ASCENT AND RETURN

ENERGY AND LIFE SUPPORT

MISSION CONTENT

COST/INCOME

OTHER ASPECTS

#5711 Re: Space Policy » The SLS: too expensive for exploration? » 2016-02-19 06:54:40

A very good post I think! 

A lot of this has to do with the amount of effort - intellectual, cultural and resourcing - you are prepared to put in.  If no one had bought cars, then the development of automobiles would have been much slower.  Likewise, with space travel, if the USSR and USA not not invested huge resources in the 50s and 60s we would not have got very far. 

There is no doubt in my mind that humans to Mars, space colonisation and off planet ISRU have been the victims of under-investment.


Tom Kalbfus wrote:
SpaceNut wrote:

I think one of the evolutions was from wood/ canvas to metals which was one thing that I can see from the images.

For sls the changes would seem to be the means to get to orbit to orbit and back with cargo loading being done by ion drive.

The next is mission duration without support from the earth surface on a regular scheduel to resupply what we need....

It just seems to me that waiting til 2043, when I will be 76 years old, seems like an awful long time to wait just to see 4 people walk on Mars. World War I is not long after Wilbur and Orville flew their Wright Flier, I think the progress they saw until 1943 was a lot more that NASA is assuming in this plan. I think by 1943, we could do a lot more than fly four people across the Atlantic.

I think the point is, I was born at an inflexion point in history, all the years before I was born, since the beginning of the 20th century was marked by the rapid advance of technology on all fronts, and suddenly after I was born, the brakes were applied and everything stayed pretty much the same, with only incremental developments in existing technology, which is what NASA seems to be assuming here. So why was the point of my birth so important as to cause the brakes to be applied soon after? Did they say, lets stop innovating? Why does the 21st century thus far look so much like the late 20th century. 50 years after the dawn of aviation, we had transcontinental flights across the Atlantic, but we're progressing through the so called "Space Age" like a crippled ant! I guess I am spoiled, throughout my childhood, I expected a great deal more technological progress that what actually occurred, children who were born around the year 2000, have grown quite accustomed to this nonprogress, it seems perfectly natural to them, while I was born when World War II was only a generation away.

http://blog.seattlepi.com/thebigblog/fi … _crop1.jpg
Seattle 1916
http://3.bp.blogspot.com/_FfetiF7C9vo/S … cident.JPG
1926
http://photos.francisfrith.com/frith/le … 87371x.jpg
1936
http://i.ebayimg.com/00/s/NjYxWDEwMjQ=/ … ~60_35.JPG
1946
http://4.bp.blogspot.com/-b3eR7Gq5i5M/U … 56+(3).jpg
1956
http://photos.francisfrith.com/frith/po … _large.jpg
1966
http://assets.blog.hemmings.com/wp-cont … 1_1500.jpg
1976
This sequence of pictures represents some of the technological progress up until I reach the age of 9
http://farm9.staticflickr.com/8096/8499 … b254_z.jpg
1986
http://www.foundsf.org/images/e/ee/Bayv … t-1996.jpg
1996
http://www.edinphoto.org.uk/0_STREET/0_ … nelson.jpg
2006
http://image.hotrod.com/f/116385254+re0 … six-15.jpg
2016
The 21st century has been rather mundane compared to what I was expecting.
http://www.seriouswonder.com/wp-content … tion-1.jpg

#5712 Re: Life support systems » Chickens » 2016-02-14 17:47:40

From my reading I draw the following conclusions:

1. Growing of salad vegetables and the like (e.g. bean shoots) in an indoor environment is relatively easy to achieve - and has been demonstrated in Antarctic bases etc.  That would be the first port of call in ISRU agriculture.

2. Other crops could be grown with relative ease but would require more labour input e.g. wheat, root crops and so on.

3.  Animal husbandry or fish farming is of another order. Fish farming is in fact pretty difficult because of the need for plentiful water supply and the need to suppress disease.  Similar problems arise with animals, especially if we are talking about enclosed air-conditioned environments.  There are many diseases that can pass from birds and mammals to humans and just trying to cope with animal feathers, hair, dander, urine and faeces is a difficult call in an indoor environment.

4.  Something small like a guinea pig might be a good first resource for animal meat on Mars. But don't neglect the possibility of insect protein.




SpaceNut wrote:

Thanks for this topic thou I can not offer much for it other than we need an over producing greenhouse  from the get go in order to not only sustain the crew in good health but also to prepare the way for husbandry.
Also inaddition to that we will need colonies of yeast, algea, bacteria for methane creation and maybe others to feast of the decaying unused garden trash and more.

#5713 Re: Life support systems » Booze » 2016-02-11 15:46:34

It could also be sold on Earth at $100,000 a bottle.

SpaceNut wrote:

The grapes should be one of those crops to try on mars as it can go along ways towards our health...not to meantion sanity....

#5714 Re: Unmanned probes » New Red Dragon Mission? » 2016-02-06 21:24:54

OK - my apologies to Spacenut and thanks for putting me right on that! smile 

GW Johnson wrote:

The Red Dragon sample return mission did not return the capsule.  Once on the surface,  the Dragon stayed there.

The capsule had installed a small rocket ascent vehicle that carried a very tiny sample.  That small rocket comes back to some high orbit about the earth,  from which it is retrieved by another,  unspecified,  craft. 

I personally have never seen any illustrations of how all this gear was to be installed.  But some versions say there was a tiny rover.  I suspect some sort of robot arm must be involved. 

GW

#5715 Re: Unmanned probes » New Red Dragon Mission? » 2016-02-06 09:03:13

SpaceNut, Not really sure why you are asking  "What thoughts do you all have to make the capsule a launch system once a sample is loaded into it as soon as its down on the surface as it will have a limit on available power." My understanding of the proposal (I may be wrong) was that it aims to land a single integral Red Dragon which can then return to LMO...and I presume the main difference from the ISS-supplying Dragon is putting more fuel/propellant on board, in order that it can retro descend (I'm guessing it the mass would be too great for a parachute landing) and then ascend from the surface. 


SpaceNut wrote:

The Red Dragon was a sample return mission louis for the topic and less about its eventual useage in LEO as a taxi.
That said what are the numbers once you remove the seats, oxygen plus tanks, life support systems extra batteries for what would have been the crews. In fact there are other mass reductions that could be made in reducing the inside structural stuff that supports a crewed controlled vehicle reducing it to an atonomous robitically controlled system.

All these things once removed make it possible to do such a mission as it give margin for the alteration and for the return vehicle to launch from its internals.....

What thoughts do you all have to make the capsule a launch system once a sample is loaded into it as soon as its down on the surface as it will have a limit on available power. We could jetison the upper part of the capsule on the way down once the retro rockets take over for landing exposing the internals for a mars sample to be placed into the returning rocket once we can load it into it.

Do we add some sort of arm to get a sample with or hope that we land close to a robot previously sent to get a cache of samples for return?

#5716 Re: Unmanned probes » New Red Dragon Mission? » 2016-02-05 17:32:26

GW Johnson wrote:

It's a little odd seeing claims that Red Dragon was a NASA idea and initiative.  That's not right.

As best I can determine,  this was a Spacex proposal for a Discovery class mission,  that was never submitted,  because NASA said it wouldn't work,  and discouraged submittal.  At least,  that part of NASA to which such proposals would go.

Looking around the on-line document trail,  I found a different group within NASA that looked at Red Dragon,  and got enthusiastic,  saying it would work.  This group seems to have since won over most of the rest of NASA.

But,  damn it,  it was a Spacex idea,  not a NASA idea.  I get pissed off when those in positions of power appropriate other people's ideas and claim credit for them.  Managers and government bureaucrats are the worst offenders. 

I see no real substantive changes to the Red Dragon idea:  Dragon v2 re-rigged to carry cargo and some other mods to land one-way on Mars with its Super Draco thrusters.  The payload originally was 1 metric ton,  over and above a fully-fueled but otherwise unloaded Dragon,  which I think might be in the vicinity of 6 tons or so.  This thing can ride Falcon-Heavy as a direct shot straight to Mars.  It is based on a really shallow direct entry angle,  or this sort of propulsive entry won't work,  not with standard tankage for the Super Dracos.   

I've seen some articles claiming up to 2 metric tons might be carried this way,  but I tend to be conservative.  I'm sticking with 1 ton until Spacex says otherwise. 

GW

Is there any reason it couldn't be used as an equivalent of an Apollo lander then if you already had a functioning hab  landed on the surface?  24 hour rest when you reach the surface. Then transfer to the hab.

#5717 Space Policy » Exploitation of resources in space - Little Luxembourg Leads » 2016-02-03 05:59:01

louis
Replies: 1

http://www.bbc.co.uk/news/science-environment-35482427

As I deduced from the Outer Space Treaty there is no bar on exploitation of resources in space.  As soon as the technology becomes affordable we will see fast-growing used of materials in space. 

The main thing I would worry about is pollution of the atmosphere is rocketry becomes a regular mode of shifting huge tonnages of metals.

The sooner we develop an electric form of space propulsion, the better.

#5718 Re: Human missions » Kbd512's human mission design for Mars » 2016-02-02 04:49:26

If anyone wants to post a mission design against the categories in this doc I set up

https://www.docdroid.net/137mm/mars-mis … f.pdf.html

...then just set the details out against the listed categories (first column) and I will update the doc.

#5719 Re: Human missions » Body clocks on Mars » 2016-01-29 19:05:47

Just going on my own vague recollections...you may well be right, but it doesn't necessarily mean the body and brain are operating proficiently when that sort of circadian drift occurs.  It's probably what happens when the body and brain aren't receiving cues from regular day/night patterns.  In other words, while we may drift to 30 hours or more, for proper functioning we need to be a lot closer to the 24 hour mark (hardly surprising given the evolutionary pressures for us to function in relation to Earth's rotational cycle) and it seems that, thankfully, Mars is just within the margin for most or a substantial part of humanity.

GW Johnson wrote:

Seems like I saw somewhere years ago something about some people who spent months isolated in a cave,  away from any light/dark signal.  Their natural circadian rhythm stretched past 30 hours.  The number I want to say I remember was about 36 hours. 

Looks like RobS in post 4 above ran across exactly the same experiment.  So I am not losing my overage mind.

GW

#5720 Re: Human missions » Body clocks on Mars » 2016-01-29 04:57:36

And very civilised it is too! The Spanish are also out on the veranda eating their evening meal at 10pm, young (well behaved) children included. A siesta approach would probably work well on Mars, where people will effectively be working probably 12-14 hour days to begin with. Much better if you split that into two work periods.

RobS wrote:

I have also heard of psychological research on subjects living in caves without clocks and no natural clues of the time of day and night. Apparently they tended to shift to a "day" of something like 30 hours.

I bet that would not be a problem, especially with a "Mediterranean" lifestyle where you eat lunch about 2, nap until 4 or 5, work a few more hours, eat supper at 9 or 10 p.m., and go to bed after midnight. When my wife and I lived in Seville, Spain, we never were able to adjust to it, but it was standard. Cities like that have 4 rush hours a day, by the way, because everyone goes home for lunch and a long nap.

#5721 Re: Human missions » Body clocks on Mars » 2016-01-28 13:02:32

Hi Robert,

I think the original article was looking at how people would experience Mars with their body clocks WITHOUT special shift systems. I am sure you are right that proper shifts could deal with any body clock issues (perhaps in tandem with artificial lighting).   

Incidentally (given your location) - is the system you describe related to the Ottawa shift system  which I recall the UK police were looking at a couple of decades ago?

RobertDyck wrote:

I have to argue against this. In first year university I was required to take an "arts credit". The course I took was first year psychology. The professor showed a number of films. One was about a psychologist that was hired to help a mining company. That mine operated 24/7 and had swing shifts. That means workers would work about 2 weeks on one shift, then switch to another. They were always tired, dragged out, unproductive. The psychologist had them go to bed as soon as their shift ended, whenever they start a new shift. Then go to bed one hour later every day, and set their alarm clock one hour later. He had supervisors schedule their shift so that just as their time to get up would bump against time to start their shift, the shift changed to 8 hours later. So the shift changed once every 8 days. The result was workers lived a 25 hour day. This ended the problems with adjustment to a new schedule. It ended the "body clock" problems. And they discovered workers actually lived better than those living a normal 24 hour day.

This was done with humans, not animals. Mars has a solar day 24 hours, 39 minutes, 35.244 seconds. That's less than the 25 hours the miners lived, and the miners handled better than a normal 24 hour day. So not a problem.

#5722 Human missions » Body clocks on Mars » 2016-01-28 09:40:32

louis
Replies: 8

http://www.sciencedaily.com/releases/20 … 90759.htm#

The takeaway point seems to be:

"But if we ever do get to the Red Planet, I suspect we will be faced with body clock problems; those people with abnormally slow body clocks would be best suited to living there."

A more positive gloss on this might be that "as long we choose the right people, there will be no problem with the human body clock on Mars"!

#5723 Re: Human missions » A solid lead on Planet X? » 2016-01-21 19:01:15

Antius wrote:

Surface escape velocity would be about three times greater than Earth, surface gravity twice as great.  At that distance, the planet probably has a dense hydrogen atmosphere.  A ground launch h2/o2 rocket would need several stages to reach orbit and the final mass ratio would be about 4000.

So we'd feel twice as heavy as we are on Earth and not have access to any meaningful solar radiation for power purposes!  This planet is not even a starter for colonisation  - even if it exists, that is (though I am sure we would all love to have some close up pics).

Come on guys,
Keep your eyes on the prize:
Mars.

#5724 Re: Human missions » A solid lead on Planet X? » 2016-01-20 13:01:33

You're getting bored with Mars?

Surely a planet that massive is inherently unsuited to human beings - given the unpleasant (for humans) G forces.

Excelsior wrote:

New evidence suggests a ninth planet lurking at the edge of the solar system

Astronomers at the California Institute of Technology announced Wednesday that they have found new evidence of a giant icy planet lurking in the darkness of our solar system far beyond the orbit of Pluto. They are calling it "Planet Nine."

Their paper, published in the Astronomical Journal, describes the planet as about five to 10 times as massive as the Earth. But the authors, astronomers Michael Brown and Konstantin Batygin, have not observed the planet directly.

Instead, they have inferred its existence from the motion of recently discovered dwarf planets and other small objects in the outer solar system. Those smaller bodies have orbits that appear to be influenced by the gravity of a hidden planet – a "massive perturber." The astronomers suggest it might have been flung into deep space long ago by the gravitational force of Jupiter or Saturn.

Telescopes on at least two continents are searching for the object, which on average is 20 times farther away than the eighth planet, Neptune. If "Planet Nine" exists, it's big. Its estimated mass would make it about two to four times the diameter of the Earth, distinguishing it as the fifth-largest planet after Jupiter, Saturn, Uranus and Neptune. But at such extreme distances, it would reflect so little sunlight that it could evade even the most powerful telescopes.

Confirmation of its existence would reconfigure the models of the solar system. Pluto, discovered in 1930, spent three-quarters of a century as the iconic ninth planet. Then, a decade ago, Pluto received a controversial demotion, in large part because of Brown.

His observations of the outer solar system identified many small worlds there – some close to the size of Pluto –and prompted the International Astronomical Union to reconsider the definition of a planet. The IAU voted to change Pluto's classification to "dwarf planet," a decision mocked repeatedly last summer when NASA's New Horizons probe flew past Pluto and revealed a world with an atmosphere, weather and a volatile and dynamically reworked surface.

A planet of that magnitude, I hope, would be a game changer, not only for exploration, but culturally. We need a frontier to remind us constantly of what really matters, what it really takes to live, and what we are really capable of.

Further, how do we get there? It seems that this would require quasi-interstellar propulsion technology. The possibilities are really exciting. It's not clear yet, and probably won't be until we get real pictures, whether its a super-earth, or a gas dwarf, and what we can do with it. But in either case, it probably has it's own harem of moons.

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