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#5926 Re: Human missions » Overview of Mission Design » 2015-02-06 12:39:55

Of course it all depends how you view these first human visitors to Mars as to who you send.

I would refer to them as colonists not as astronauts.

Therefore my emphasis would be more on mining, construction, engineering, electrical maintenance and farming. Ideally, i would like the first colonists to be experiment with a range of ISRU techniques and also undertaking detailed medical assessments of their own performance.

Detailed exploration of geology and so on, can wait a few years would be my view - though obviously some geological knowledge will be needed to find minerals and water.

The important thing for me is to get a continuous colony established.

#5927 Re: Human missions » Overview of Mission Design » 2015-02-05 16:23:10

Thanks Robert, that's very helpful.

I agree with you about the doctor being replaced by a paramedic if necessary. Things have moved on a lot. We now have computer systems that are better at diagnosis than the average GP (general doctor). We also have some surgical procedures that can be carried out by robots. 

Anyway, let's forget the idea of a "risk free" mission.  We can minimise many risks. But ultimately the solution may be to carry a lot of morphine.

Is this basically your own mission design you are quoting?



RobertDyck wrote:

Mission size: I support 4 people in one craft. Like Mars Direct. As Dr. Zubrin and his partner David Baker said, that would be 2 scientists and 2 engineers. The engineers would fix stuff. Dr. Zubrin got pressure from NASA to increase crew size to 6, including one medical doctor. There was some discussion to compromise: 5 including the doctor. But I argue astronauts can be trained as paramedics, and with modern high tech medical equipment they can do whatever is required.

Transit: convention chemical rocket. SLS with LH2/LOX upper stage for transit to Mars. ISPP for return, so methane/LOX. I propose one SLS launch for the Mars Ascent Vehicle, sent unmanned. Then a cargo lander with lab and pressurized rover with backup life support. Then assemble the crew vehicle in LEO, using ISS as construction shack. The Interplanetary Transit Vehicle (ITV) would be reusable, used for transit from ISS to high Mars orbit. The MAV would have oversize fuel tanks so it could be the TEI stage. The ITV would have the lander/hab attached. This has the advantage that if a free return is required, all food and supplies for the surface stay and the return trip are still with you. A free return will not be 6 months, that trajectory will take a lot longer. The lander will include an open rover in case they land too far from the MAV. And yes, I do prefer artificial gravity, but if NASA really panics about that, the ITV can use zero-G.

Entry/Descent/Landing: Aerocapture into Mars orbit. The ITV will also aerocapture into Earth orbit on return, then aerobrake down to LEO, before finally using rockets to rendezvous with ISS and dock. Because aerocapture is tricky, the ITV will require an emergency escape pod that can directly enter Earth's atmosphere. That would be a Dragon spacecraft. Lander EDL: carbon fibre umbrella style heat shield that NASA is currently working on, then parachute, and finally landing rockets with legs. Rather than a single large landing engine like the Apollo LM, instead use rocket engines around the periphery like the sky-crane of the Curiosity Rover. The lander/hab would be smaller than Mars Direct, because the lab would not be included. The lab would be pre-landed. The crew lander could be a capsule with inflatable habitat. This lab would also be inflatable. An inflatable requires a storage bag with micrometeoroid shield for transit, but once erected on Mars it does not require a micrometeoroid shield. Instead it requires a thermal insulation compatible with Mars atmosphere, and a dust/scuff layer to protect against dust storms and astronauts rubbing against it. The best external layer for Mars would be Tennara architectural fabric, which is the same material as the outermost layer of Orthofabric, but without the Nomex/Kevlar backing. Or should we just use Orthofabric itself?

Energy and Life Support: the MAV will use a small nuclear reactor for ISPP. Specifically the SAFE-400 because it's already developed. The lab and  habitat will use solar: PV without concentrator. That's the same mix as Mars Direct. Life support with be recycling, but with a mix of technologies with ability to mix&match components for even more options. ISRU for a couple of the backups. One mode: the MAV will harvest CO2 from Mars atomsphere for ISPP, one component of recycling life support is direct CO2 electrolysis, so as back these can be combined to produce oxygen from Mars atmosphere. Another backup, harvest Mars permafrost, melt and filter for clean water, run through the electrolysis tank of primary life support. So oxygen from Mars permafrost.

Mission Content: I argue that so much time has been wasted and so many unmanned rovers sent that we need to start building the permanent base with the first human mission. Each mission will land at the same location. Initial exploration from base via rover, but eventually add a land-on-your-tail rocket for extended exploration range. Explore, do science, but also grow food in greenhouses, and use ISRU for construction material to expand the base. The first two missions will use a cargo lander to pre-land a lab, but subsequent missions will use the labs left there. Each mission will land a new habitat, so with all missions landing at the same location this will build up quite a base.

Cost: I've tried to estimate cost, but that keeps changing. That's a long discussion.

#5928 Human missions » Overview of Mission Design » 2015-02-05 07:19:03

louis
Replies: 38

I'm finding some of the discussions a bit confusing at the moment!

Wondered whether it was possible to construct an overview with the help of people here.

Feel free to answer/comment underneath and if I get enough responses I will construct an overview that people might find helpful.  There might be key factors in mission design that I have left out - feel free to point those out.

I am particularly interested in who is proposing what - so if you can indicate that, that will be v. helpful.

MISSION SIZE

What options are being given serious consideration?  Who is backing which option as far as we know?

One person mission?  (Usually associated with a one way ticket mission?)

Two person?

Three person?

Four person? 

Is anyone proposing a double mission (my own favourite) e.g. 2x 3 people = 6 in total - going in on basically two identical craft (bit like Viking if you like).

Which agencies are backing these?

TRANSIT TO MARS


1. What are thought to be the main potential methods?


A. Conventional rocket?

What different types of fuel might be used?

B.  Nuclear power?

C.  Solar electric?

Am I right in thinking only conventional rocket has so far been used for missions to Mars?

2.   What different configuration are there for the Mars Transit?

I would favour (a) Lander/Ascent vehicle (b) supply module (c) Bigelow style Hab (d) Transit rocket - assembled in LEO.


3.  If there is assembly involved what are the options - where best to assemble: LEO or  elswhere.

4.  Who is proposing artificial gravity ?

5.  What are the options for radiation protection.



ENTRY, DESCENT AND LANDING

1.  What are the different proposals for entry and descent?

2. What are the different strategies for landing?

Parachute/ablative shield (inflated or non-inflated)/retro rockets?

3.  How much tonnage do the different proposals envisage landing?

4.  How much do the different proposals rely on pre-landing of cargo.


ENERGY AND LIFE SUPPORT


1. What are the options for energy production ? Solar (PV Panelling - concentrated or not); solar heating; nuclear; wind? Any others?

2. How will life support be maintained ?  By imported material or through ISRU?  What will be the balance between the two.


MISSION CONTENT


1. What is the mission content? 

Flags and footprints?

Exploration?

Food production?

Mining and ISRU?

Rocket fuel production for return journey?

Any others?

2. Will there be a separate hab or will the crew stay in the lander?

3. What will be the ascent options (if ascent forms part of the mission).


COST 

What are the cost estimates for the various proposals?

To what extent are these covered by income generation e.g. commercial sponsorship.

How will net costs be covered (e.g. one agency or several?)

#5929 Re: Human missions » Living Energetically on Mars » 2015-01-28 17:50:50

JCO wrote:

There is a post in the transportation topics about riding bikes on Mars. For pure transportation purposes a human powered vehicle will likely be able to move at an equal speed and with the same safety as any other power source. It also provides another benefit that could be very valuable to explorers and colonist on Mars, exercise. The prolonged exertion of human powered vehicle could be very effective at combating muscle and bone loss.

That brings me to the point of this post. I think the key to humans health on missions will be identifying tasks where human effort will be as effective or more effective than a machine. The challenge would be to identify ways to efficiently make use of human effort. At the moment I can think of one other task that may fit into this category, digging. Humans may actually prove to be more efficient at digging in the regolith then a machine that could conveniently transported to Mars. Because of the difference in gravity digging on Mars may feel more like shoveling snow and any rocks smaller than a person would be fairly easy to move.

What do other think would be tasks that would make good use of human power?

You mean digging outside?  I think you'll need help from a microwave blade - otherwise you would be trying to dig in frozen regolith. Maybe sand I suppose could be moved even in frozen conditions.

#5930 Re: Martian Politics and Economy » Martian Exports » 2015-01-27 19:25:56

JCO wrote:

I think the best way to think of what Mars will export is to look back to the colonization of the new world. Most of the exports that fueled the colonies were items that could not be gotten from anyplace but the new world. Spain's gold rush was relatively short lived and did not create many long lasting colonies. No commodity that can be found on Earth will likely be worth shipping back to Earth. So what does Mars have that Earth does not, martian geology. Just like the new world the colonies will not be funded by mundane rare commodities but by unique luxury goods. Anything that could be fashioned into jewelry from martian 'rocks' will be worth orders of magnitude more than the identical item of terrestrial origin. Anything that has a unique make up and an appealing appearance will be worth shipping back to Earth. Martian granite and marble will be more valuable than platinum. It will be shipped back to Earth to floor the most exclusive hotels and the most expensive mansions.


Yes I've referenced Mars jewelry before now.

Also I think after a few years a Mars colony could for instance assemble Rolexes on Mars - incorporating say some Mars gold, if it exists - the connotations of Mars as a "male" planet would add to the appeal for the super-rich man. I could see those going for $100,000 each.  Ten little Rolexes might have a sale value of $1million back on Earth.   But there might be a market for a 1000 per annum back on Earth.

There might well be a market as well for Mars textiles (v. lightweight gossamer type products) and Mars luxury agricultural products e.g. Mars wine.

When one thinks of the global world GDP on Earth, we are only talking about skimming off a tiny proportion to make a viable Mars colony of say 100,000. A surplus of a couple of billion might be enough to sustain them. 

Once the colony is established selling life support for visiting film and documentary crews, and mega rich "gap year" students will generating huge amounts of money.

#5931 Re: Human missions » Boeing's plan for Mars » 2015-01-27 02:54:51

kbd - I think you misunderstood my point.  What we don't have info on is how well people perform when put into mass-adjusted suits on a low G body like Mars or the Moon after prolonged exposure to zero G (we know they recover well on Earth, and we can probably hazard a guess they will perform quite will with special suits to simulate gravity on Mars or Moon). So you need the preceding phase of zero G to simulate the journey to Mars. That's why I argue for an analogue mission to the Moon - which is only 3 or 4 days away (so a rescue mission could be mounted).

Actually I am confused by your post - you seem to be both arguing against me and agreeing with me!





kbd512 wrote:
louis wrote:

I doubt anyone is going to send people to Mars without an analogue mission to the moon.   I agree with Impaler that AG is likely to prove a very expensive diversion in terms of both money and time.

Flying a transit habitat around the moon for six months won't tell us anything that we don't already know about microgravity.

AG is too expensive or complicated whereas active radiation shielding is some sort of requirement for a Mars mission?  The tech for effective particle shields to deflect protons with gigavolt energies or better is guaranteed to be far more expensive and heavier than AG.  All the concepts I've seen had impressive power requirements.  Are we going to power the propulsion system with our solar panels or use it to deflect radiation?

If we stop using soda cans for habitats, that'd be a good first step towards reducing radiation exposure.  There are lots of better materials for absorbing radiation than aluminum.

With respect to AG, humans weren't designed for microgravity environments and there's no getting around that.  Microgravity poses actual health problems and just because someone is ambulatory doesn't mean the effects aren't real or lasting.  All we need is for someone's corneas to be adversely affected on the surface of Mars to put all the ridiculous hand wringing about the effects of radiation into context.

louis wrote:

We can establish how people will react by taking them to the Moon first in lunar orbit for 6 months, until landing on the lunar surface, where they can work in 1G weighted suits and their health can be assessed.  The Mars habitat can be tested at the same time.

We already have plenty of data to discern the health effects of microgravity and radiation.  We don't need any more human guinea pigs to tell us what we already know.

louis wrote:

I think they will be able to cope. But we have to test it first without taking them to Mars would be my view.

I don't want to find out how well the crew fares when they're tens of millions of miles from home.

#5932 Re: Human missions » Mars One » 2015-01-26 09:28:46

SpaceNut wrote:

This power is no issue has been suggested before but I think that its going to depend on what choices are made for each leg of the mission to Mars.

http://en.wikipedia.org/wiki/Electrical … ce_Station

http://en.wikipedia.org/wiki/Integrated … subsystems

http://www.nasa.gov/images/content/3610 … s-xltn.jpg

Two blankets of solar cells make up a solar array wing, or SAW. Each wing is 115 feet long by 38 feet wide. Each SAW weighs more than 2,400 pounds and uses 32,800 solar array cells. Altogether, the four sets of arrays can generate 84 to 120 kilowatts of electricity. The solar arrays produce more power than the station needs at one time for station systems and experiments. When the station is in sunlight, about 60 percent of the electricity that the solar arrays generate is used to charge the station's batteries. The battery charge/discharge units (BCDUs) regulate the amount of charge put into the battery. Each BCDU can regulate discharge current from two battery ORUs, and can provide up to 6.6 kW to the Space Station. During insolation, the BCDU provides charge current to the batteries and controls the amount of battery overcharge. Each day, the BCDU and batteries undergo sixteen charge/discharge cycles. The Space Station has 24 BCDUs, each weighing 100 kg. Each battery assembly consist of 38 lightweight Nickel Hydrogen cells and associated electrical and mechanical equipment. Each battery assembly has a nameplate capacity of 81 A·hr and 4 kW·hr. This power is fed to the ISS via the BCDU and DCSU respectively. The batteries have a design life of 6.5 years and can exceed 38,000 charge/discharge cycles at 35% depth of discharge. Each battery measures 40” by 36” by 18” and weighs 375 pounds.

http://en.wikipedia.org/wiki/File:Truss_breakdown.png

http://en.wikipedia.org/wiki/File:Elect … bution.png

Sure seems like to get the power that we need is going to be quite massive.....

A few points:

1.  I think the mass of the ISS's SAWs would be much greater than the equivalent required on Mars.  PV panelling can be much more lightweight on Mars because the ground can keep it in position i.e. they don't have to be part of rigid fixed wing structure. 

2.  Battery technology has moved on a lot since the batteries were installed on the ISS. So again the batteries should be much lighter.

3.  We can use solar concentrators on Mars - that would be difficult in ISS orbit.

#5933 Re: Human missions » Mars One » 2015-01-25 18:02:31

RobertDyck wrote:

Collecting CO2 from Mars atmosphere is fairly straight-forward. At night it's so cold it's almost enough to freeze as dry ice. MACDOF is designed to chill Mars atmosphere those last few degrees each night so it does form a block of dry ice. Then seal, and warm to sublimate during the day. This self-pressurizes. And isolates CO2. Robert Zubrin and his company designed that.

I gave a presentation at a Mars Society convention on harvesting other gasses from Mars atmosphere. Other gasses require a lot more power; primarily for the pump to pressurize. It was written as PowerPoint slides with notes. The following link is that PowerPoint converted to a Word document. It isn't pretty, hasn't been formatted as a paper for publication, just slides with presentation notes. And I still have the spreadsheet that I used to calculate the numbers.
ISRU Atmosphere Harvesting

My point is you want to keep life support as closed as possible. It doesn't have to be completely closed. In fact non-food crops will consume CO2, and produce excess oxygen. Whether you grow wood, bamboo, hemp, or cotton, anything not eaten or decomposed, will fix carbon. As long as that carbon is not burned, it produces excess oxygen. Food crops will produce non-edible plant matter, but that can be composted to become fertilizer. But composting takes time, so initially the greenhouse will produce copious quantities of excess oxygen. So it can't be completely closed, but should be as much as possible to reduce power.


"To reduce power" - but is power a real problem?   I think domestically we each use about 1 kW per hour in our homes on average ...that's 6 Kws per hour for a six person mission or 144 KwHs per day. Remember though we do lots of things we won't need to do on Mars. We won't need to use hair dryers or watch very large TV screens or use energy-thirsty washing machines.  We will need to heat our homes, but equally we will be living in the best insulated habs in the solar system!  So a lot of our earthbound energy usage could be converted into energy work in farm habs etc.




Maybe you would need something like 700 sq. metres of PV panelling, or 26 metres by 26 metres.  You'll probably need a margin of safety for dust storm conditions. Remember, as well you can send the

#5934 Re: Not So Free Chat » Impact of Post-scarcity economics » 2015-01-25 16:41:23

GW Johnson wrote:

In all societies during and since the stone age (and probably before),  people have had to have a "job" of some sort (generalized definition) in order to live.  It is hardly possible for a single individual to supply himself with all his needs for all of his life.  We learned to live cooperatively in groups,  each doing different "jobs" so that all could live better,  long before we were ever human.  Many species have done this,  because it works.

The flip side is that you don't eat (etc) if you don't do your job.  I don't care what economic system you want to talk about,  that's still fundamentally true.  So,  everybody has to have a "job" to do.  Period.  That's just life.

OK,  now automate all the jobs with robots of one sort or another.  So what are we humans supposed to do for a living?  Didja ever think of that?  I think robots are fine,  as long as there is something else useful for us humans to do for a living.  When there isn't,  I am dead set against automation.  Period. 

Western civilization has been down this road several times before.  Each time it did not turn out well. 

The last time is when they automated manufacturing to the greatest extent possible,  without any thought at any level anywhere in society,  as to what else the fired workers would do for a living.  What they couldn't automate,  they outsourced overseas to the slave labor societies. 

That is precisely why for the so-called "middle class",  it now takes 2 full-time workers to support a family,  instead of the 1 full-time worker that it took when I was a boy. 

"Automation for profit without regard to the human consequences" is the most precise way of saying what I so strenuously object to.  And that's precisely what is being discussed above,  in this thread. 

Beware,  you are planning your own demises,  should this speculation actually come to pass. 

GW


Speculation this is...but look at the way things have gone recently.   We see houses with solar panels, supplying their own energy needs...3D printing...through our  computers we can Google a world of information and - as a for instance - become better acquainted with a disease than our local doctors (GPs as we call them in the UK)...We already have our own warehousing and cold storage facilities in our houses (fridges and freezers).

I don't think there's any doubt about the way the technology is heading: towards a huge increase in home-based self-sufficiency.

I see a future for fresh food grown at home, including - in time - "lab meat"  (sure they'll come up with a nicer name for it).

In terms of how you distribute the productive potential of a society that has always been a political matter.   

What would people do if there time wasn't taken up with work? 

I guess much as now - leisure, education and volunteer time would expand to take up the hours created by the shrinkage of work.  I think people's health would generally benefit.

I don't think work would disappear completely.  It would probably become just  small part of our lives for most people.  We might work a couple of days a week in order to acquire the cash for the things we need money to buy.

#5935 Re: Human missions » Boeing's plan for Mars » 2015-01-25 15:00:46

kbd512 wrote:
Impaler wrote:

Artificial gravity sounds nice, but we have enough ISS experience to send people up for 6 months and have them come down into Earth gravity and be good to go in a few days, they are not cripples as some people like to exaggerate.  In other words we can get to Mars in ISS derived habs and just recuperate for a tiny fraction of the surface stay time upon landing in lander/habitat, a trivial operational constraint that allows us to dispense with all the engineering of spinning stuff.

That's just what I want.  A group of astronauts who can't walk without fainting after they've landed on another planet thirty million miles from Earth.  All the engineering of spinning a wheel is too complicated?  Wow.  Maybe we should just be content here on Earth.


I doubt anyone is going to send people to Mars without an analogue mission to the moon.   I agree with Impaler that AG is likely to prove a very expensive diversion in terms of both money and time. 

We can establish how people will react by taking them to the Moon first in lunar orbit for 6 months, until landing on the lunar surface, where they can work in 1G weighted suits and their health can be assessed.  The Mars habitat can be tested at the same time.

I think they will be able to cope. But we have to test it first without taking them to Mars would be my view.

#5936 Re: Space Policy » Investment in Space vs Earth » 2015-01-20 18:19:11

I used to wake up with frost on the inside of the windows as a child! LOL  And that was in the UK!

We need to reform taxation and benefits in the UK  as well as Canada. 

Personally I would go for: a flat rate income tax (no allowances); a universal citizen's benefit (to restore a strong work incentive, along with the flat income tax); a graduated property tax; a differential sales tax; and a financial transaction tax.  It's too easy for the rich and oligarchs living in the UK to dodge income tax.

Space investment is vital to economic development.  In fact the UK has huge a space satellite sector.  Apparently, because we were one of the first countries to develop satellite TV, we got a lead in the satellite economic sector generally and so became a world leader.

If I was in control of space policy in the UK I'd be looking to develop space tourism with a focus on lunar tourism.  I know Branson's run in to difficulties but I would link with Musk to achieve this.


RobertDyck wrote:

In a "Human Missions" discussion thread...

louis wrote:

What's lacking is the political will (Obama in particular doesn't do space - he's a Chicago street activist and they were always complaining about the space budget not being spent on the poor).

This concerns me. I'm all for helping the little guy, but space is about opening new frontiers and new resources. Opening new resources makes the entire economy richer. The poor need consideration, but obsessing about them to the exclusion of opening new resources simply makes everyone poor.

I am concerned about what is going on in Canada. When the current Conservative government was elected in January 2006, the cancelled the last cut by the Liberal administration to personal income taxes. Then a year later brought back that same tax cut, claiming they had cut taxes. It was only 0.5%, but bringing back a cut they cancelled is not a cut. There has been no cuts to personal income tax since. Instead they cut corporate taxes. The Liberal administration passed a law to cancel corporate capital tax, but the effective date was after the 2006 election, so the Conservatives have claimed credit. The Liberals stated their intent to cancel corporate surtax, but during the 2006 election they were in the process of abolishing corporate capital tax. One at a time; if you cut taxes too deeply too quickly, you abolish the surplus. The surplus is used to pay down the debt, which reduces debt service charges (interest). That reduced interest is what allows the government to reduce taxes. So cuts have to be slow. Cutting too quickly kills the goose that lays the golden eggs. The goose is the surplus, and golden eggs are tax cuts. But the Conservatives didn't stop there, they cut corporate tax down to 15%. Personal income tax at the lowest income bracket is 15%. That means multi-billion dollar corporations are paying taxes at the same rate as individuals with income below the poverty line. That's absurd. That does have to change.

My proposal for Canada is:

  • Cut personal income tax by 2% points in every income bracket. For the lowest income bracket that reduces from 15% to 13%. Effective January 1st 2016. That's New Years Day following the next federal election. Election day is scheduled for October 19, 2015.

  • Increase corporate income tax by 1% point that same day, January 1st, 2016. From 15% to 16%.

  • Shift tax on dividends from personal income tax to corporate. Again January 1st 2016. That means corporations will no longer be able to deduct what they pay in dividends from taxable income, effectively charging corporate income tax on dividends. Corporations will be prohibited from deducting anything from the dividend cheque; the corporation pays, now shareholders. Of course how much a corporation pays in dividends is up to them. And dividend cheques from a corporation that pays corporate income tax to Canada will not be included in taxable income for personal income tax. Making a dividend cheque tax free. But that would not apply to dividends from foreign corporations, because they don't pay corporate income tax to Canada. The Canada Revenue Agency has to get their tax money somewhere.

  • Increase GST (Canada's federal sales tax) by 1%, from 5% to 6%, effective April 1st, 2016. That gives retailers time to adjust their cash registers, and April 1st is the beginning of the Canadian federal government's fiscal year. Increase a further 1% effective July 1st, raising from 6% to 7%. The GST was 7% on election day 2006, so this just puts it back to what it was.
    Note: Personal income tax cut by 2%, GST raised by 2%. But income tax is on all your income while GST is only on some things. And the raise in GST will be delayed, so taxpayers get a break.

  • The GST Credit is a rebate cheque mailed to low income taxpayers once per quarter. Effective April 1st (again start of the federal government's fiscal year), change that. Change it to a line item added to your paycheque. Instead of taking the annual amount, dividing by 4 and mailing a cheque, instead divide by how many paycheques you get per year, add that to every paycheque. So instead of 1/4 every 3rd month, you could get 1/26 bi-weekly. Current line items on a pay stub are deductions, but this would be added to your paycheque. And employers would net this out with income tax withholding. Most importantly, the total amount paid per year would double. Yes, this off-loads expenses to employers, and passes on those savings to taxpayers. If an employer complains, my response is "Suck it up buttercup."
    Anyone not employed but receiving Employment Insurance benefits would receive this on their EI cheque instead. Anyone not employed and not receiving EI, but retired and receiving Canada Pension Plan benefits would get it on their CPP cheque. Anyone not getting any of that but getting provincial welfare, would get it on their welfare cheque. Anyone who doesn't get any of that would get their GST Credit on the following year's income tax refund.
    And to ensure no one gets more than one payment, all employers will be required to register employee's Social Insurance Number (SIN) (Canadian equivalent to Social Security Number) with a website of the Canada Revenue Agency. If that SIN is already assigned to get the GST Credit elsewhere, or doesn't qualify to receive the GST Credit, the employer will be told "No". No explanation why, just "No".

  • The following year, effective January 1st 2017, federal personal income tax will be cut another 2% points in every income bracket. For the lowest income bracket that cuts from 13% to 11%.

  • To pay for that, the same day, January 1st 2017, corporate income tax will raise by 2%, from 16% to 18%.

  • The year after that, January 1st 2018, personal income tax cut another 1% point in every income bracket. The lowest income bracket will be cut from 11% to 10%.

  • To pay for that, the same January 1st 2018, corporate income tax increase 1%, from 18% to 19%.

Then leave it there. On election day 2006, corporate income tax was 21%, plus corporate surtax, plus corporate capital tax. After all this, corporate income tax will be 19%, and no corporate capital tax or surtax. That's lower and that's enough. Individuals below the poverty line will pay 10% income tax; that's a tithe.

I also want to restore the surplus, treat the federal debt like a mortgage, pay the whole damn thing off. Once the entire Canadian federal debt is gone, completely abolish federal personal income tax. Of course the GST Credit would have to go at the same time as federal personal income tax. One major purpose to the GST Credit is incentive to file your income tax return. If you don't file, you don't get the GST Credit. Employment Insurance (EI) and Canada Pension Plan (CPP) together are the equivalent to Social Security. Those premiums pay for those programs, so the premiums have to stay. But no increase, no decrease, no change what so ever. Provincial income tax is under authority of provincial governments, so anyone who wants to change that has to talk to their provincial politicians. This plan doesn't change that. Corporate income tax and GST itself will stay at the level I just listed. The real reason for shifting dividends from personal income tax to corporate is so when federal personal income tax is completely abolished, dividends stay taxed. So this isn't magic. But if you look at your pay stub, look at the box that says "Federal Income Tax". That will be gone; your paycheque will be that much bigger because it simply won't be deducted.

Further spending cuts: In late 2005, the Liberal administration was a minority government, so to stay in power they needed support from at least one other political party. The Conservative Party was trying to force an election, so the Liberals tried to placate the NDP. In Canada, the Liberal Party is not as "liberal" as the Republicans in the United States use the word. The Liberal Party tries to be fiscally responsible. However, the New Democratic Party is socialist. In an effort to placate the NDP, in late 2005 they introduced a bill to create a national childcare program. It didn't pass, and the Conservative administration has instead created the "Universal Child Care Benefit for Children Under the Age of 6". Yea, long name. It's a $100 cheque mailed to parents every month. But it's considered taxable income. After tax that works out to $16 per week. Not much, but in 2011 cost the government $2.8 billion. They haven't included a line item for that program since. During the 2011 election, the Liberal calculated the cost of their childcare program: $0.5 billion the first year, rising each year until the 4th it would cost $1 billion, then capped at $1 billion thereafter. Now the Conservatives have promised to increase the cheques to $160 per month, parents would get the money starting this July. The election is October: can you say "buying votes"? I knew you could. My idea is replace the Conservative childcare plan with the Liberal one. Assuming the cost of the Conservative plan hasn't increase since 2011 (it probably has), then the 60% increase means $4.48 billion per year. Replacing that with a $0.5% billion program saves about $4 billion the first year alone. And the Liberal plan is more effective. It entails training unemployed people receiving EI benefits or welfare to establish a home business providing childcare. That gets individuals off social assistance, instead self-employed.

Isn't that more effective?  This doesn't cut funding from space. Again, space is an investment. There's lots of new land on Mars. Lots of metals in asteroids. Lots of resources to make society richer.

Another perspective. My mother was a pre-school child during the Great Depression of the 1930s. She described growing up in a small town in southern Manitoba. Here in Canada, in the province where I now live. Her parents had a tiny house with a coal-and-wood stove; no furnace. They had to stoke the stove before going to bed at night, and during the coldest nights of winter had to get up during the night to re-stoke the stove. She often woke to find her bed sheets frozen to the bed. When they got up, they ran to the stove to warm up. They drew water in a bucket from a hand-pump; they didn't have running water. Their father (my grandfather) hunted for meat: deer, duck, geese, occasionally smaller animals. They had a small subsistence farm with a few acres of potatoes, vegetables, and some chickens. Canada didn't have a national healthcare system at that time. Their mother (my grandmother) got serious complications from childbirth, worse with each child. She stopped after 4 children. Her husband (my grandfather) had to pay punishing hospital bills, so they were dirt poor until those bills were paid. After the Great Depression they recovered; had a small restaurant for a few years, then my grandfather built houses until he retired. But now compare the so-called "poor" of today with how my own mother grew up. Are they really poor? It's all relative.

#5937 Re: Human missions » Yet another Mars architecture » 2015-01-20 04:56:25

RobertDyck wrote:

Ok. I quoted data from Encyclopedia Astronautica. Checking the SpaceX website, to get data directly from the horse's mouth:
Payload to LEO: 53,000kg (116,845 lb)
Payload to GTO: 21,200kg (46,738 lb)
Payload to Mars: 13,200kg (29,101 lb)
Status: Expected Launch in 2015

So now the relevant question: what is the price of Falcon Heavy, Altas V 552, and Delta IV Heavy? The Wikipedia page you linked cites

The published prices for Falcon Heavy launches have moved some from year to year, with announced prices for the various versions of Falcon Heavy priced at US$80-125 million in 2011, US$83-128 million in 2012, US$77.1-135 million in 2013, and US$85 million for up to 6,400 kg to GTO (with no published price for heavier GTO or any LEO payload) in 2014.

And Wikipedia for the other launch vehicles:

In 2013, the cost for an Atlas V 541 launch to GTO (including launch services, payload processing, launch vehicle integration mission, unique launch site ground support and tracking, data and telemetry services) was about $223 million (inflation adjusted $226 million in 2015). In 2014 the ESA contracted ULA to launch the Solar Orbiter for around $173 million. Since about 2005 Atlas V has not been cost-competitive for most commercial launches, where launch costs were about $100 million per satellite to GTO in 2013.

Delta IV Heavy: Cost per launch $375 million (2014)

With that lift mass, one launch of Falcon Heavy might be able to lift both the ITV and Mars lander with unpressurized rover (open rover). That would eliminate one Falcon 9 launch for the first mission. Subsequent missions would reuse the ITV, so launch the lander with rover on Falcon 9.

It may be interesting to work out the exactly mass, so we can calculate the exact TMI stage mass. Could we get it small enough for a single Falcon Heavy? To replace the SLS Block 1. Or would splitting the TMI stage into two work? To replace one SLS Block 1 with two Falcon Heavy. Which would have the lower total cost?

I have always tended to multiply the launch costs to get a Mars mission. I did that based on some published project costs as against launch costs.

Obviously, even if you are using rockets and some other equipment that have been through the development phase, you are still going to have development, planning and mission control costs.  On billion dollars might pay for 5,000 people for ONE year (engineers and scientists being pretty highly paid, and there being lots of on costs - pensions, health care and so on). Or 500 for ten years.  500 people is not so many on the payroll.   Once you start thinking in terms of 24/7 cover at a mission control, well you have to divide the number of people by four (three shifts and other cover) - so if your mission control had 50 people, you would need 200 on the payroll.

I think we probably need something like 20-40 tonnes on the Mars surface, for a return mission.   I would hazard the total costs would be much higher than perhaps you are suggesting - a minimum of several billion, but I'd like to see maybe $20billion invested over 20 years to do it right - with plenty of pre-missions. That's only $2 billion per anum - a joint enterprise of NASA, ESA, JAXA and others should easily be able to handle that funding. What's lacking is the political will (Obama in particular doesn't do space - he's a Chicago street activist and they were always complaining about the space budget not being spent on the poor).

#5938 Unmanned probes » Mars One's favoured Seed Project. » 2015-01-17 08:46:27

louis
Replies: 1

http://www.mars-one.com/news/press-rele … -to-mars-i

I quite like this Mars One project as an opener. 

Do we know if they have the funding to achieve this? 

How much would it cost do you think? Could you do it for $200million I wonder.   How much would Space X charge you get your Mars Probe into LEO? 

It looks like they would have a simultaneous Comsat mission?

#5939 Re: Interplanetary transportation » SpaceX Falcon 9R launch » 2015-01-10 19:44:59

GW Johnson wrote:

I see in today's news that Falcon-9/Dragon launched successfully to ISS.  The attempt to land and recover the 1st stage was only partially successful.  They actually did hit the recovery barge,  but they crashed hard upon it,  near as I can tell.  Still,  they hit the target at all,  that's significant in and of itself. 

GW


How does the barge work?   Virtually any sea conditions will involve some pitch and roll. I'm assuming they must have some sort of gyro system on board that attempts to compensate and create a stable surface?  Or maybe it has very strong magnets to hold the legs as they touch down? But that seems unlikely.

#5940 Re: Human missions » Food for Thought, what does a garden need to grow » 2015-01-02 17:28:02

There are many societies around the world where people basically subsist on far fewer food sources. 

Personally I think to begin with the emphasis should be on a pretty limited range of foods: dwarf buckwheat is my favourite for a grain - it's pretty versatile. You don't really need a full range of salad vegetables. Just ensure you are a growing a dark green leaf (much more nutritious than those watery lettuces), tomatoes and onions.

Potatoes are very nutritious of course.

A fatty fruit like an avocado vegetable is useful.     

Mushrooms are quite a good meat substitute. 

I think guinea pig raising should be tried early on...I don't see any reason why that shouldn't succeed.

Although we can begin with hydroponic agriculture, I'd be particularly interested in artificial soil creation on Mars: grinding down rock, mixing in sand and clay from Mars, adding human/guinea pig faeces, adding various minerals found on Mars, and adding food waste/leaf mulch.   Might be useful for growing plants like potatoes.

#5941 Re: Space Policy » The Outer Space Treaty » 2014-12-31 12:42:55

Terraformer wrote:

No, *sovereignty* cannot be claimed. However, the ownership of habitats can be - much the case in Antarctica and on the sea. So if you want to own a patch of land on Luna or Mars, you have to actually build something over it. In other words, the standard for property ownership is the one that most libertarians and anarchists agree on - perhaps the only time states have ever done such a thing.

If a government were to "license" land, it would be claiming sovereignty, just as it would be if it "licensed" international waters.

The signatories of the treaty undertake to supervise private sector activity.  I think that gives justification for a licensing system.

#5942 Re: Space Policy » The Outer Space Treaty » 2014-12-31 05:07:35

I have seen nothing that dissuades me from my view: that property rights cannot be established on celestial bodies under the OST but there would be nothing to prevent a national government instituting a system of licensing of land in a particular area on the Moon or on Mars. Effectively, the licensing system would become a de facto form of leaseholding.

The Moon Treaty seems so poorly ratified as to be irrelevant to the discussion.

#5943 Re: Life on Mars » Curiosity and the life on Mars Question. » 2014-12-26 20:46:59

Aren't we in the area of media management here?  I did wonder about that methane announcement and now, given your post, it seems to me it was clearly just a NASA media management exercise. We've known about methane on Mars for a long time - and I think ESA have confirmed it as well.  Clearly it sounds like NASA are now just looking to justify their expenditure on Opportunity.

We all know that the real way forward is to get people on Mars who can do close up observation and effectively direct robots at the surface

#5944 Re: Planetary transportation » Martian Transportation Infrastructure » 2014-12-22 20:04:44

JoshNH4H wrote:

Something to keep in mind with transportation on Mars is that we want to keep it as simple as possible.  We need to ask ourselves:  How little energy can we use, how weak can we make our motors, etc.

My proposal is this:  Robotic driving would be easiest with a "rail" made of bricks laid down for the car to follow.  This is solely a guide rail and the entire weight and maneuvering forces on the car would be on the ground.  The car can travel at speeds as low as 5 m/s (18 kph; 11 mph) or less.  The path can be designed to have inclines below 10 degrees.  Maybe it's fine if the cars turn off at night.  Maybe on an incline the vehicle will "gear down" so as to use less power by going slower.

But, thinking about it, chemical fuels are probably the way to go.  They have really high volumetric and specific energy densities and can be pretty easy to manufacture and store.  Oxidizer is kind of tricky, but we don't necessarily need a very powerful one.  Chlorine is a liquid at ambient martian temperatures, for example.  We don't need to worry about polluting Mars.  In fact, CF4 is a very powerful greenhouse gas.  The best argument for not releasing it is that it may be worth keeping the chlorine for reuse.  Oxygen isn't as good because it's not liquid at Mars pressures, but you could get a reasonably high density by pressurizing.  Then there are compounds like Ammonium Nitrate, which are relatively safe, oxidizing solids that can also be dissolved in water. 

My point is this: Keep it simple and low-powered, and chemical, and it'll work for a long time at low cost.

I agree with that approach. But simpler than bricks are white lines at intervals. Robot vehicles have no problem following those.

#5945 Re: Life support systems » Turning structures like Mount Sharp into Martian Cities. » 2014-12-21 19:57:35

SpaceNut wrote:

With Sandstone comes The cave digger, Ra Paulette: Hewing art from the very landscape

One small opening pales in comparison to the cavern he's dug inside. It took close to 900 hours to dig.

http://cbsnews2.cbsistatic.com/hub/i/r/ … es-003.jpg

The sense of being underground with light streaming in, the intimacy of being in a cave, yet the columns end up very large, sometimes 30, 40 feet high.

http://cbsnews1.cbsistatic.com/hub/i/r/ … ave-01.jpg

http://www.racavedigger.com/racavedigge … _Home.html

Very nice! 

This is one of the ways we could generate money for the Mars community.  There are many super-rich artists on planet Earth - they would pay many millions to be the first to display works of art on Mars.  So, take with you a robot "sculptor" that can carve out the sandstone according to a computer-control programme sent by the artist from Earth.

I would suggest that would be a brilliant start for a new Mars community, to create a sandstone art gallery - in time it would become a huge tourist attraction on Mars.

#5946 Re: Life support systems » Turning structures like Mount Sharp into Martian Cities. » 2014-12-21 19:54:33

Void wrote:

Louis,

I want to make sure that I did not intend the "Screaming Child" thing to indicate you or any of your associates.  I am really thinking of the human race as a whole, and much less people like you.

Please don't take insult.

No problem - but Titan can wait. Let's focus on Mars for a few decades.  It would be an incredible achievement to have a basically, or potentially,  self-sufficient civilisation established on another planet.

#5947 Re: Life support systems » Turning structures like Mount Sharp into Martian Cities. » 2014-12-20 05:59:17

I don't think power is really an issue for any size of settlement we can imagine developing in the first 100 years. There is plenty of free open land on which to site PV panelling.  And PV power can be used to make methane using ISRU.  Certainly it wouldn't be a problem for any community up to around 100,000 - which I think of as the population target for creating a fully self-sufficient off-Earth human civilisation.

With PV power, 3D printers and ISRU, we can achieve self-sufficiency.



Void wrote:

That's funny, we are both implicated.

I do think sandstone is a very good option though, particularly if the site takes care of other requirements, and reduces hazards (Seasonal cold, carbon dioxide snow loads, and so on).

One other factor I did not yet include is that if it is true that fusion energy were to appear, this would be just the place for it I think.

http://www.lockheedmartin.com/us/produc … usion.html

http://www.technologyreview.com/news/53 … n-machine/

I really am an easy sucker for flash news some times, but lockheed martin being the source apparently, I might be forgiven for being hopeful.


http://www.realclearscience.com/2012/12 … 50332.html

Samples from a small mound of dust on Mars contain five times as much ‘heavy water’, than you would find in a similar sample on Earth.

The dust was analysed by the three soil experiments on board NASA’s latest rover on the planet, Curiosity.

So really, if you had a sandstone city, and atmospheric gasses, and had solved the problem of a water supply, .....and had fusion power on Mars where heavy water must be easier to get than on Earth.

Then you almost could live inside the mountain with artificial lights until the planet was suitably terraformed to have a biosphere.  Of course why would you ignor other sources of energy though.

#5948 Re: Life support systems » Turning structures like Mount Sharp into Martian Cities. » 2014-12-19 14:57:13

"but for some reason lava tubes on Mars are larger".  Gravity??

I am always slightly distrustful of lava tubes...don't they end up with a lot of jagged edges?  That just feels counterintuitive for human missions where safety is a prime concern. 


RobertDyck wrote:

Salt deposits: Probably near dried-up bodies of water, such as shores of the dried-up ocean basin. And what was the deepest part of the ocean; as it dried up the salt water would flow there before finally evaporating. But that implies little chance for water flow through salt deposits.

Earth has plate tectonics, so everything is constantly moving. Mars never did have plate tectonics. The islands of Hawaii formed by volcanic eruption from a hot-spot in the mantle. As the tectonic plate moved the island off the hot-spot, the volcano stopped erupting. Then a new volcano would form over the hot-spot, creating a new island. Then ocean waves slowly eroded erode old islands. But this never happened on Mars. Volcanoes at Tharsis just built up to huge size. And Tharsis is on the opposite side from Hellas Basin, probably the shock wave from the asteroid impact that created Hellas caused the volcanoes of Tharsis. All this means no salt deposits that can later be dissolved to form caves. No process to build up then tear down.

We don't know if limestone deposits formed. On Earth, igneous rock eroded by lowing water into clay. Alkali metals dissolved from that rock washed into the oceans: sodium, potassium, magnesium, calcium. Early Earth had a thick CO2 atmosphere, so a lot of CO2 dissolved into the ocean creating carbonic acid. That's a weak acid, but dissolved carbonic will combine with calcium to form calcite, or with magnesium and calcium to form dolomite. Those two minerals precipitate out of solution, forming limestone. Today Earth doesn't have a CO2 atmosphere, so this process doesn't happen any more. Today coral other life forms make calcium based skeletons, which accumulate to form coral reefs. But bulk limestone was formed by early Earth through this non-biologic process. We find calcite and dolomite in Mars soil. It's part of the dust, they haven't found limestone deposits; at least not yet. I'm sure the chemical process was the same, the question was whether these minerals were formed in rivers and streams, or Mars ancient ocean. Could there be limestone deposits at the bottom of the ancient ocean?

Limestone caves: there wasn't much time for one of these to form. When the ocean started drying up, it's possible a part of limestone left on land could have had water percolate through to the lowered ocean. But that wasn't much time. Look at the ancient shore line, but there may be no limestone caves. We haven't even found bulk limestone yet.

But orbiters have discovered lava tubes. These form when a lava river flows down a volcano hillside. Cooling lava forms a solid crust, which acts as insulation so remaining lava underneath stays hot longer. This forms a tube of molten lava. When the volcano stops, the honey-like lava flows down hill, emptying the lava tube. Some lava will solidify on the tube floor. We have lava tubes on Earth, but for some reason lava tubes on Mars are larger.

Wikipedia: Martian lava tube
http://upload.wikimedia.org/wikipedia/c … a_tube.jpg
http://upload.wikimedia.org/wikipedia/c … t_crop.jpg
http://media1.s-nbcnews.com/j/MSNBC/Com … id-6x2.jpg
http://www.newscientist.com/data/images … -1_650.jpg

#5949 Re: Life support systems » Turning structures like Mount Sharp into Martian Cities. » 2014-12-18 13:08:36

Are there likely to be salt deposits on Mars?   Salt caves on Earth can be huge:

http://therockspa.com/Halotherapy-History

#5950 Re: Life support systems » Turning structures like Mount Sharp into Martian Cities. » 2014-12-17 18:58:09

I would draw a distinction between early settlement and later settlement.

In the early missions,  digging out caves in sandstone would be a distraction in my view.  Easier to import habs or use cut and cover to create hab space using ISRU.

However, as population grows, digging into caves may make more sense in that, with supports, you can probably create quite large structures.

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