Dennis Tito, space-tourist and uber-rich dude, is planning a Mars Fly-by. The 2018 Launch promises a 501 day Free-Return trajectory – a great big loop past Mars (ain’t stopping) and return to Earth for a high-speed re-entry. Such a mission – if successful – will be a proof of concept that Mars flights aren’t impossible for humans. Actual landing flights will take ~180-130 days in orbital trajectories, either way, so they will require even less zero-gee exposure (if spin-gravity isn’t used) than Tito’s proposal. People have stayed in orbit for much longer than that, and have soaked up even more cosmic-rays than that. So, as Robert Zubrin has noted more than once, there is no real space-medicine case against flights to Mars.
Dennis Tito, Space Tourist, and colleagues are holding a press-conference and a quick search of talks at the IEEE Aerospace Conference in Montana brings up Tito’s “8.0105 Feasibility Analysis for a Manned Mars Free Return Mission in 2018″, which discusses (probably) a 501 day Free-Return mission to fly-by Mars, launching in 2018. Of course the usual nay-sayers and craven know-it-alls have predicted probably insanity if a crew of two are cramped up in a SpaceX “Dragon” Capsule for 501 days, but I am sure the wannabe interplanetary astro-tourists are well aware of the challenges ahead. Such daring requires a certain monomaniacal insanity to even contemplate, so I have no doubts that it can be achieved by sufficiently willing and mentally tough individuals.
Of course the supplies and living quarters will need something more like this, than a basic “Dragon”:
The expandable Habitat isn’t basic SpaceX equipment, but a Bigelow Aerospace derived concept. The ISS is due to get such an expandable “Trans-Hab” like extension and Bigelow Aerospace have orbited mini-space stations based on their designs, as well as having full-scale mock-ups tested here on Earth.
Just to be clear, the current proposal does not seem to be a landing mission. In 2011 Robert Zubrin proposed a bare-bones mission to Mars, to land and live for ~18 months, which I discussed here: SpaceX to Mars! Here’s How… . One cute feature, perhaps a nod to the Australian Mars Society’s effort, was the rolled out solar-arrays to power the MAV fuelling system. That’s only more and more viable as the ability to make flexible solar-cells increases all the time.
There’s nothing stopping, but will and perceived feasibility, the launch of a Mars Base One in time for the 50th Anniversary of the First Moon Landing and certainly no excuse not to do so before the 50th Anniversary of the Last Moon Landing. Humanity’s Nations need an ambition far more creative and positive than being the Top Dog in Geo-Political Arena. If the Nations don’t do it, as an aspirational goal for their people, then I hope some billionaires will step to the challenge. A Trail-Blazer effort – a successful one – like a fly-by and teleoperated activities on Mars, will change the risk-assessment. People, flesh and blood, CAN do this.
The Medician Stars, as Galileo dubbed his discovery in orbit around Jupiter, reimagined as terraformed worlds by 1Wyrmshadow1, on his Deviant Art page. James Oberg discussed their terraforming in his (now classic) “New Earths” (1981), as has Martin Beech in his more recent “Terraforming: The Creating of Habitable Worlds” (2009) and Martyn Fogg in “Terraforming: Engineering Planetary Environments” (1995). The first, semi-serious discussion, was fictional – Robert Heinlein’s “Farmer in the Sky” (serialised as “Satellite Scout” in 1950, then novelised in 1953.) Heinlein’s tale began with Ganymede being given an oxygen atmosphere busted out of ice on the ground, via total-annihilation powered systems. Heinlein is vague on details – he knew the ingredients, not the details. So he had the moon being kept warm via “the Heat-Trap” and the ice being lysed by some energy delivery system. The story begins long after the process had progressed to a colony of 15,000 dirt-farmers slowly converting the place into living room for an over-flowing Earth.
Of course Heinlein had to fudge a few details. Even in 1950 Ganymede was suspected to be rather too low density to be as rocky as Heinlein describes. The real Ganymede is half ice. Not a total disaster. If only the outer-layers melted and the topography was kind, then water would pool in the lower parts and the meteoritic dust in the crust would form a layer of soil over it. Such a world would need to stay, on average, cool, but parts would be warm enough for water and vegetation. Ice warms slowly – witness the permafrost under the tundra of northern Europe. Given a low enough average temperature and enough salts in the ice and the stuff will remain stable. But beware TOO MUCH Global Warming…
There are Lies, Damned Lies and Statistics. The worst lies are told with seemingly significant statistics. Though I’m not a statistician, I am an Australian, and the (ab)use of Australian crime statistics by the NRA in the USA is downright annoying. Less annoying, but more worrying, is how people swallow such crud holus bolus.
However, let’s flip this around. In the USA the homicide rate, from all causes, is about 5 times higher than in Australia, per 100,000 of population. And 2/3rds of homicides are via guns. I can understand how the right to self-defense with guns of one’s choice makes people feel more secure, whether they are or not. But the ease of access combined with the devastating collateral damage power of firearms makes the USA, overall, 500% deadlier than Australia – or even their neighbour, Canada. So I can understand the existential dread that drives people in the States to bear arms, but that fear seems to be more of a self-fulfilling prophecy.
My Mormon friend, Jen, pointed me to a very interesting web-site with all this gun homicide data. Worth a look…
I am not asking my friends in the USA to give up their firearms – hell, I’d pack heat too – but they need to start asking questions about how their “freedom” affects everyone around them. Sure, bad people use guns, when good people don’t. But that Gun Culture comes with a price paid in blood. Denying that fact is suicidal ignorance.
Turning a source of heat – such as concentrated sunlight – into useful power (say, electrical power) is not an easy proposition. There’s a dizzying array of options – thermal engines using different thermodynamic cycles, photovoltaic arrays, thermoelectrics and thermionic conversion. The last was used extensively in early space power generators using small reactors or radioisotope heat sources, but left behind by thermoelectrics and Stirling cycle free-piston systems in more recent work. Now a new approach to “thermionic” conversion, focussing on electrons (thus thermoelectronic), has shown promising behaviour in experiments and out-standing performance in theory.
Thermionics previously had efficiency limitations due to “space current” – build-ups of electrons mutually repelling each other and choking the flow of current – so the new system uses external electric or magnetic fields to get the electrons going in the right direction. The system promises a high fraction of the Carnot Limit can be converted directly into electrical power. The Carnot Limit is a measure of how much useful work can be extracted from a thermal cycle – if the heat source temperature is Tin and the heat-sink temperature is Tout, then the Carnot Limit is:
CL = (Tin-Tout)/Tin
…say the source is 2000 K and the sink is 500 K, then the Carnot Limit is (1500/2000) = 0.75. In practice realistic thermal engines achieve a fraction of the Limit and thermionics & thermoelectrics achieve a low fraction. Efficiencies of 5-10% are typical. The new thermoelectronic approach promises efficiencies in the high 40-50% range, achieving the latter by acting as a “topping cycle” to a lower temperature steam system. For example a coal furnace burns at ~1500 C (1773 K), but a steam turbine runs at 700 C (973 K) and outputs at 200 C (473 K). Thus there’s significant loss due to the mismatch between furnace and steam power-cycle. A thermoelectronic converter covering the 1773-973 K range will add significantly to the overall power extracted by the power-plant pushing its efficiency above 50%. In this case a 45% efficient coal plant can be pushed to 54%, thus increasing the power output for no additional fuel costs and NO MOVING PARTS.
Switching to solar-power applications, imagine a thermoelectronic converter at the centre of a concentrator system which focuses sunlight to 500 times its normal intensity (temp ~1900 K.) By using a Photon Enhanced Thermionic Emission (a cousin of the Photoelectric effect) the system can convert raw sunlight to electrical power at over 40% efficiency. While maintaining a hard vacuum around the emitter-collector system is difficult here on Earth (but easy enough given the right engineering) imagine such a system in space! Hard vacuum everywhere! Even the densest squall of the Solar-Wind is a harder vacuum than a Thermoelectronic system needs here on Earth. Concentrators have to remain pointed at the Sun, but this isn’t excessively onerous engineering either.
One problem is the trick of efficiently losing excess heat to maintain the temperature differential that drives the system, but even this isn’t intractable engineering in space. Given the right “heat-pipes” the whole system can be built without moving parts, eliminating the main failure-point for mechanical thermal-cycle converter systems that have been proposed in the past.
Using Carbon-NanoTube (CNT) sheets that we can make now, we might push towards ~2,200 km/s. Of course there will be structural mass and the payload reducing the top speed – thus we might hit ~1,800 km/s tops with CNT sheets, if made perfectly reflective. Even for lower reflectivity the speed will be about ~1000-1500 km/s.
How hard can we push it? A 1999 study by Dean Spieth, Robert Zubrin & Cindy Christensen for NASA’s Institute of Advanced Concepts (NIAC), which can be found here, examined using CNTs arranged in a spaced-out grid. One of the curiosities of optical theory is that, for a given range of wavelengths, the reflective material doesn’t have to be an unbroken sheet – it can be an open-grid.
Computing the reflectivity of such things is difficult – best to make it and measure it – but estimates of how a CNT grid would perform suggests that a CNT sail might accelerate at ~18 m/s2 at 1 AU from the Sun, implying a final speed of 2,320 km/s. Dropping inwards and launching from 0.019 AU would mean a final speed of 16,835 km/s (0.056c), allowing a probe to reach Alpha Centauri in just 78 years, propelled by sunlight alone!
To send people, rather than rugged robots, a different approach will be needed – to be discussed in Part 3.
Carbon is the material of the Future. Graphite, graphene, bucky-balls and nanotubes all have amazing properties. And then there’s diamond – which seems to come in several varieties, albeit rare and/or theoretical.
Making enough of any of the allotropes – different carbon forms – is rather tricky, aside from raw graphite, which can be mined. Diamonds fortunately can be made fairly easily these days – very pure diamond crystals can be (almost) made as large as one likes. Thus Jewel Diamonds, the kind De Beers sets the standard for, have to be slightly impure crystals, as they’re thus provably natural.
Carbon nanotubes are proving easier to make and to make into useful forms. One application caught my eye:
…which have the rather amazing property of being strong and yet massing just ~27 milligrams per square metre. If we can dope it (add a sprinkling of other elements) to make it more reflective, then it makes rather impressive solar-sail material. Sunlight’s pressure – as felt by a reflective surface facing flat to the Sun – is about 1/650 th of the sun’s gravity, so creating lift against the Sun’s gravity requires very large, light sheets. And doped CNT sheets – if 100% reflective – would experience a lift factor (ratio of light-pressure to the sail’s own weight) of 57 (!)
In theory that means a suitably steered solar-sail made of CNT sheet could send itself away from Earth’s orbit and reach a final speed of 42*sqrt(57-1) km/s ~ 315 km/s. If it swooped past Jupiter then swung in hard for the Sun, scooting past at 0.019 AU, then it would recede at ~2,200 km/s.
We’ll ponder that some more next time.
Just beyond Neptune is the Kuiper Belt, a torus of comet-like objects, which includes a few dwarf-planets like the Pluto-Charon dual-planet system. Despite being lumped together under one monicker, the Belt is composed of several different families of objects, which have quite different orbital properties. Some are locked in place by the gravity of the big planets, mostly Neptune, while others are destined to head in towards the Sun, while some show signs of being scattered into the vastness beyond. Patryk Lykawka is a one researcher who has puzzled over this dark, lonely region, and has tried to model exactly how it has become the way it is today. Over the last two decades there has been a slow revolution in our understanding of how the Big Planets, the Gas Giants, formed. They almost certainly did not begin life in their present orbits – instead they migrated outwards from a formation region closer to the Sun. To do so millions of planetoids on near-misses with the Gas Giants tugged them gently outwards over millions of years. We know what happened to the Gas Giants, but what of the planetoids? A fraction today form the Kuiper Belt and the Oort Cloud beyond it (how many Plutos exist out there?) But a mystery remains, which Lykawka convincingly solves in his latest monograph via an additional “Super-Planetoid”, a planet between 0.3-0.7 Earth masses, now orbiting somewhere just beyond the Belt.
Such an object would be a sample of the objects that formed the Gas Giants, a so-called “Planetary Embryo”. Based on the ice and silicate mix present in the moons of the Gas Giants, the object would probably be half ice, half silicates/metals, like a giant version of Ganymede. However such an object would also have gained a significant atmosphere, unlike smaller bodies, and being cast so far from the Sun, it would have retained it even if it was composed of the primordial hydrogen/helium mix of the Gas Giants themselves. This has two potentially very interesting consequences. David Stephenson, in 1998, speculated on interstellar planets with thick hydrogen atmospheres able to keep a liquid-water ocean warm from geophysical heat-sources alone. Work by Eric Gaidos and Raymond Pierrehumbert suggests hydrogen greenhouse planets are a viable option in any system once past about ~2.0 AU. A precondition that obtains for Lykawka’s hypothetical Super Trans-Neptunian Object.
So instead of a giant Ganymede the object is more like Kainui, from Hal Clement’s last novel, “Noise”. Kainui is a “hot Ganymede”, a water planet with sufficiently low gravity that the global ocean hasn’t been compressed into Ice VII in its very depths. Kainui’s ocean is in a continual state of violent agitation, lethal to humans without special noise-proof suits, but Lykawka’s Super-TNO would probably be wet beneath its dense atmosphere, warmed by a trickle of heat from its core and the distant Sun.
Gravitational perturbation studies of planetary orbits by Lorenzo Iorio constrain the orbital distance of such a body to roughly where Lykawka suggests it should be. A Mars-mass object (0.1 Earth-masses) would exist between 150-250 AU, while a 0.7 Earth-mass body would be between 250-450 AU. If we place it at ~300 AU, then its equilibrium temperature, based on sunlight alone, would be somewhere below 16 K. That’s close to the triple-point of hydrogen (13.84 K @ 0.0704 bar), suggesting a frozen planet would result. However geophysical heat, from radioactive decay of potassium, uranium and thorium, could elevate the equilibrium temperature to over ~20.4 K, hydrogen’s boiling point at 1 atm pressure. Thus a thick hydrogen atmosphere should stay gaseous.
To keep liquid water warm enough (~273 K) at the surface, the surface pressure will need to be ~1,000 bar, the equivalent of the bottom of Earth’s oceans. An ammonia-water eutectic mixture would be liquid at ~100 bars and 176 K. With a higher rock fraction and higher radioactive isotope levels (as seen in comets, for example), liquid water might be possible at ~300 bars. Such a warm ocean would seem enticingly accessible since a variety of submarines and ROVs operate in the ocean at such pressures regularly. While the prospects for life seem dim, the variety of chemosynthetic life-styles amongst bacteria suggest we shouldn’t be too hasty about dismissing the possibility.
A primordial atmosphere also invites thoughts of mining the helium for that rare isotope, helium-3. At 0.3 Earth masses and 1:3 ratio of ice to rock, such a body has 75% Earth’s radius and just 40% the gravitational potential at its surface – even less at the top of the atmosphere. Such a planet would be incredibly straight-forward to mine and condensing helium-3 out of the mix would be made even easier by the ~30-40 K temperature at the 1 bar pressure level. There’s no simple relationship between the size of a planet and its spin rate, but assuming Earth’s early spin rate of 12 hours, then the synchronous orbital radius is just 2 Earth radii above the operating altitude of a mining platform. A space-elevator system would be straight-forward to implement, unlike the Gas Giants or even Earth.
Travelling to 300 AU is a non-trivial task, ten-times the distance to Neptune. A minimum-energy Hohmann trajectory would take 923 years, while a parabolic orbit would do the trip in 390 years. Voyager’s 15 km/s interstellar cruise speed would mean a trip of 95 years. A nuclear saltwater rocket, with an exhaust velocity of 4,725 km/s, could be used to accelerate to 3,000 km/s, then flip and brake at the destination. The trip would take six months, which is speedy by comparison.