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  • JEAN LEGALL: Good afternoon, ladies and

  • gentlemen. I'm Jean LeGall. I'm

  • President of the French Space Agency and

  • the President elect of the International

  • Astronautical Federation, and it is my

  • pleasure to welcome you here at the 67th

  • International Astronautical Congress.

  • Elon Musk is founder, C.E.O., and lead

  • designer of SpaceX. Elon founded SpaceX

  • in 2002 with the goal of revolutionizing

  • space technology and ultimately enabling

  • humans to become a multiplanetary

  • species, and that's the plan he's going

  • to lay out for us today.

  • SpaceX has had a number of firsts

  • including as the first private company

  • to deliver cargo to and from the

  • International Space Station and the

  • first entity to land a nautical thrust

  • booster back on land and on ships out at

  • sea.

  • Please join me in welcoming Elon Musk.

  • [APPLAUSE].

  • ELON MUSK: Thank you. Thank you very

  • much for having me. I look forward to

  • talking about the SpaceX Mars

  • architecture. And what I really want to

  • achieve here is to make Mars seem

  • possible, make it seem as though it's

  • something that we can do in our

  • lifetimes and that you can go. And is

  • there really a way that anyone can go if

  • they wanted to?

  • I think that's really the important

  • thing.

  • So, I mean, first of all, why go

  • anywhere?

  • Right?

  • I think there are really two fundamental

  • paths. History is going to bifurcate

  • along two directions. One path is we

  • stay on Earth forever and then there

  • will be some eventual extinction event.

  • I don't have an immediate doomsday

  • prophecy, but eventually history

  • suggests there will be some doomsday

  • event. The alternative is to become a

  • space-faring civilization and a

  • multiplanet species, which I hope you

  • agree that is the right way to go.

  • Yes?

  • [APPLAUSE].

  • That's what we want.

  • [APPLAUSE].

  • Yeah. So how do we figure out how to

  • take you to Mars and create a

  • self-sustaining city, a city that is not

  • really an outpost but can become a

  • planet in its own right and thus we can

  • become a truly multiplanet species?

  • You know, sometimes people wonder, Well,

  • what about other places in the solar

  • system?

  • Why Mars?

  • Well, just to sort of put things into

  • perspective, this is -- this is what --

  • this is an actual scale of what the

  • solar system looks like. So we're

  • currently in the third little rock from

  • the left. That's Earth. Yeah, exactly.

  • And our goal is to go to the fourth rock

  • on the left. That's Mars. But you can

  • get a sense for the real scale of the

  • solar system, how big the sun is and

  • Jupiter, Neptune, Saturn, Uranus. And

  • then the little guys on the right are

  • Pluto and friends.

  • This sort of helps to see, it's not

  • quite to scale, but it gives you a

  • better sense for where things are. So

  • our options for going to -- for becoming

  • a multiplanet species within our solar

  • system are limited. We have, in terms of

  • nearby options, we've got Venus. But

  • Venus is a high-pressure -- super

  • high-pressure hot acid bath. So that

  • would be a tricky one. Venus is not at

  • all like the goddess. This is not in no

  • way similar to the actual goddess.

  • So it is really difficult to make things

  • work on Venus.

  • Mercury is also way too close to the

  • sun. We could go potentially on to one

  • of the moons of Jupiter or Saturn, but

  • those are quite far out, much further

  • from the sun, a lot harder to get to.

  • Really, it leaves us with one option if

  • we want to become a multiplanet

  • civilization, and that's Mars. We could

  • conceivably go to our moon, and I have

  • nothing against going to the moon, but I

  • think it's challenging to become

  • multiplanetary on the moon because it's

  • much smaller than a planet. It doesn't

  • have any atmosphere. It's not as

  • resource rich as Mars. It has a 28-day

  • day, whereas the Mars day is 24 1/2

  • hours. And in general, Mars is far

  • better suited to ultimately scale up to

  • a self-sustaining civilization.

  • Just to give some comparison between the

  • two planets, there are actually --

  • they're remarkably close in a lot of

  • ways. In fact, we now believe that early

  • Mars was a lot like Earth. And, in fact,

  • if we could warm Mars up, we would, once

  • again, have a thick -- a thick

  • atmosphere and liquid oceans.

  • So, where things are right now, Mars is

  • about half again as far from the sun as

  • Earth. So it has decent sunlight. It's a

  • little cold, but we can warm it up. It

  • has a very helpful atmosphere which, in

  • the case of Mars being primarily CO2

  • with some nitrogen and argon and a few

  • other trace elements, means that we can

  • grow plants on Mars just by compressing

  • the atmosphere. And it has nitrogen,

  • too, which is also very important for

  • growing plants.

  • It will be quite fun to be on Mars,

  • because you will have gravity which is

  • about 37% that of Earth, so you will be

  • able to lift heavy things and bound

  • around and have a lot of fun. And the

  • day is remarkably close to that of

  • Earth.

  • So we just need to change that bottom

  • row, because currently we have 7 billion

  • people on Earth and zero on Mars.

  • So there's been a lot of great work by

  • NASA and other organizations in early

  • exploration of Mars and understanding

  • what Mars is like, where could we land,

  • what's the composition of the

  • atmosphere, where is there water, or

  • ice, we should say. And we need to go

  • from these early exploration missions to

  • actually building a city.

  • The issue that we have today is that if

  • you look at a Venn diagram, there's no

  • intersection of sets of people who want

  • to go and can afford to go. In fact,

  • right now you cannot go to Mars for

  • infinite money. Using traditional

  • methods, you know, if taking sort of a

  • holistic style approach, an optimistic

  • cost number would be about $10 billion

  • per person. For example, the Apollo

  • program, the cost estimates are

  • somewhere between $100 billion to $200

  • billion in current-year dollars, and we

  • sent 12 people to the surface of the

  • moon, which was an incredible thing and

  • I think probably one of the greatest

  • achievements of humanity.

  • But that's -- that's a steep price to

  • pay for a ticket. That's why these

  • circles only just barely touch. So you

  • can't create a self-sustaining

  • civilization if the ticket price is $10

  • billion a person. What we need is a

  • closer -- is to move those circles

  • together. And if we can get the cost of

  • moving to Mars to be roughly equivalent

  • to a median house price in the U.S.,

  • which is around $200,000, then I think

  • the probability of establishing a

  • self-sustaining civilization is very

  • high. I think it would almost certainly

  • occur -- not everyone would want to go.

  • In fact, I think a relatively small

  • number of people from Earth would want

  • to go. But enough would want to go and

  • who could afford the trip that it would

  • happen. And people could get

  • sponsorship. And I think it gets to the

  • point where almost anyone, if they saved

  • up and this was their goal, they could

  • ultimately save up enough money to buy a

  • ticket and move to Mars. And Mars would

  • have labor shortage for a long time so

  • jobs would not be in short supply.

  • But it is a bit tricky because we have

  • to figure out how to improve the cost of

  • trips to Mars by 5 million percent. So

  • this is -- this is not easy. I mean,

  • it's -- and it sounds like virtually

  • impossible but I think there are ways to

  • do it. This translates to an improvement

  • of approximately 4 1/2 orders of

  • magnitude.

  • These are the key elements that are

  • needed in order to achieve the 4 1/2

  • order of magnitude improvement. Most of

  • the improvement would come from full

  • reusability, somewhere between 2 and 2

  • 1/2 orders of magnitude. And then the

  • other two orders of magnitude would come

  • from refilling in orbit, propellant

  • production on Mars and choosing the

  • right propellant. So I'm going to go

  • into detail on all of those.

  • Full reusability is really the super

  • hard one. It's very difficult to achieve

  • reusability for even an orbital system,

  • and that challenge becomes even

  • substantially greater for a system that

  • has to go to another planet. But as an

  • example of the difference between

  • reusability and expendability in

  • aircraft -- and you can actually use any

  • form of transport. You could say a car,

  • bicycle, horse. If they were single-use,

  • almost no one would use them. It would

  • be too expensive. But with frequent

  • flights, you can take something like an

  • aircraft that costs $90 million and if

  • it was single use, you would have to pay

  • half a million dollars per flight. But

  • you can actually buy a ticket on

  • Southwest right now from L.A. to Vegas

  • for $43, including taxes. So that's -- I

  • mean, that's a massive improvement.

  • Right there it's showing a four order of

  • magnitude improvement.

  • Now this is harder -- the reusability

  • doesn't apply quite as much to Mars

  • because the number of times they can

  • reuse the spaceship is -- the spaceship

  • part of the system is less often because

  • the Earth-Mars rendezvous only occurs

  • every -- every 26 months.

  • So you get to use the spaceship part

  • roughly every two years.

  • Now, you get to use the booster and the

  • tanker as frequently as you'd like. And

  • so it makes -- that's why it makes a lot

  • of sense to load the spaceship into

  • orbit with essentially tanks dry and

  • have it have really quite big tanks that

  • you then use the booster and tanker to

  • refill while it's in orbit and maximize

  • the payload of the spaceships that when

  • it goes to Mars, you really have a very

  • large payload capability.

  • So as I said, refilling in orbit is one

  • of the essential elements of this.

  • Without refilling in orbit, you would

  • have a half order of magnitude impact

  • roughly on the cost. By "half order of

  • magnitude," I think the audience mostly

  • knows, but what that means is each order

  • of magnitude is a factor of ten. So not

  • refilling in orbit would mean a 500%,

  • roughly, increase in the cost per

  • ticket.

  • It also allows us to build a smaller

  • vehicle and lower the development cost,

  • although this vehicle is quite big. But

  • it would be much harder to build

  • something that's five to ten times the

  • size. And it also reduces the

  • sensitivity of performance

  • characteristics of the booster rocket

  • and tanker. So if there's a shortfall in

  • the performance of any of the elements,

  • you can actually make up for it by

  • having one or two extra refilling trips

  • to the spaceship. So this is -- it's

  • very important for reducing the

  • susceptibility of the system to a

  • performance shortfall.

  • And then producing propellants on Mars

  • is actually also very obviously

  • important. Again, if we didn't do this,

  • it would have at least a half order of

  • magnitude increase in the -- in the cost

  • of a trip. So 500% increase in the cost

  • of the trip. And it would be pretty

  • absurd to try to build a city on Mars if

  • your spaceships just kept staying on

  • Mars and not going back to Earth. you

  • would have this, like, massive graveyard

  • of ships. You would have to, like, do

  • something with them. So it really

  • wouldn't make sense to -- to leave your

  • spaceships on Mars. You really want to

  • build a propellant plant on Mars and

  • send the ships back.

  • So and Mars happens to work out well for

  • that because it has a CO2 atmosphere,

  • it's got water rights in the soil, and

  • with H2O and CO2 you can produce CH4,

  • methane, and oxygen, O2.

  • So picking the right propellant is also

  • important.

  • Think of this as maybe there's three

  • main choices. And they have their

  • merits, but kerosene or rocket

  • propellant-grade kerosene which is also

  • what jets use.

  • Rockets use a very expensive form of

  • highly refined form of jet fuel

  • essentially which is a form of kerosene.

  • It helps keep the vehicle size small,

  • but because it's a very specialized form

  • of jet fuel, it's quite expensive. Your

  • reusability potential is lower. Very

  • difficult to make this on Mars, because

  • there's no oil.

  • So really quite difficult to make the

  • propellant on Mars. And then propellant

  • transfer is pretty good but not great.

  • Hydrogen, although it has a high

  • specific impulse, is very expensive,

  • incredibly difficult to keep from

  • boiling off because liquid hydrogen is

  • very close to absolute zero as a liquid.

  • So the insulation required is

  • tremendous, and the cost of -- the

  • energy cost on Mars of producing and

  • storing hydrogen is very high.

  • So when we looked at the overall system

  • optimization, it was clear to us that

  • methane actually was the clear winner.

  • So it would require maybe anywhere from

  • 50 to 60% of the energy on Mars to

  • refill propellants using the propellant

  • depot. And just the technical challenges

  • are a lot easier.

  • So we think -- we think methane is

  • actually better on just really almost

  • across the board.

  • And we started off initially thinking

  • that hydrogen would make sense, but

  • ultimately came to the conclusion that

  • the best way to optimize the cost per

  • unit mass to Mars and back is to use an

  • all-methane system, or technically

  • deep-cryo Methalox.

  • So those are the four elements that need

  • to be achieved. So whatever system is

  • designed, whether by SpaceX or anyone,

  • we think these are the four features

  • that need to be addressed in order for

  • the system to really achieve a low cost

  • per -- a cost per ton to be of service

  • on Mars.

  • This is a simulation about the overall

  • system.

  • (Music).

  • (Video).

  • [APPLAUSE].

  • So what you saw there is really quite

  • close to what we will actually build. It

  • will look almost exactly what you saw --

  • like what you saw. So this is not an

  • artist's impression. The simulation was

  • actually made from the SpaceX

  • engineering CAD models. So this is not

  • -- you know, it's not just, well, this

  • is what it might look like. This is what

  • we plan to try to make it look like.

  • In the video, you got a sense for what

  • this system mock architecture looks

  • like. The rocket booster and the

  • spaceship take off, loads the spaceship

  • into orbit. The rocket booster then

  • comes back. It comes back quite quickly,

  • within about 20 minutes. And so it can

  • actually launch the tanker version of

  • the spacecraft, which is essentially the

  • same as the -- as the spaceship but

  • filling up the unpressurized and

  • pressurized cargo areas with propellant

  • tanks. So they look almost identical.

  • This also helps slow the development

  • cost, which obviously will not be small.

  • And then the propellant tanker goes up.

  • It will go -- actually, it will go up

  • multiple times, anywhere from three to

  • five times, to fill the tanks of the

  • spaceship in orbit. And then once the

  • spaceship is -- the tanks are full, the

  • cargo has been transferred, and we reach

  • the Mars rendezvous timing, which as I

  • mentioned is roughly every 26 months,

  • that's when the ship would depart.

  • Now, over time there would be many

  • spaceships. You would ultimately have, I

  • think, upwards of a thousand or more

  • spaceships waiting in orbit. And so the

  • Mars colonial fleet would depart en

  • masse. Kind of like Battlestar

  • Galactica, if you have seen that thing.

  • Good show. So it's a bit like that.

  • But it actually makes sense to load the

  • spaceships into orbit because you have

  • got two years to do so and then make

  • frequent use of the booster and the

  • tanker to get really heavy reuse out of

  • those. And then with the spaceship you

  • get less reuse because you have to

  • prepare for how long is it going to

  • last?

  • Well, maybe 30 years. So that might be

  • 12 to maybe 15 flights with the

  • spaceship at most. So you really want to

  • maximize the cargo of the spaceship and

  • use the booster and the tanker a lot.

  • So the ship goes to Mars, gets

  • replenished, and then returns to Earth.

  • So going into some of the details of the

  • vehicle design and performance -- and

  • I'm going to gloss over -- I'll only

  • talk a little bit about the technical

  • details in the actual presentation, and

  • then I'll leave the detailed technical

  • questions to the Q and A that follows.

  • This is to give you a sense of size.

  • It's quite big.

  • (Laughter).

  • [APPLAUSE].

  • The funny thing is in the long-term, the

  • ships will be even bigger than this.

  • This will be relatively small compared

  • to the Mars interplanetary ships of the

  • future. But it kind of needs to be about

  • this size because in order to fit a

  • hundred people or thereabouts in the

  • pressurized section plus carry the

  • luggage and all of the unpressurized

  • cargo to build propellant plants and

  • build everything from iron foundries to

  • pizza joints to you name it, we need to

  • carry a lot of cargo.

  • So it really needs to be roughly on this

  • sort of magnitude, because if we say

  • like the -- that same amount of

  • threshold for a self-sustaining city on

  • Mars for civilization would be a million

  • people. If you only go every two years,

  • if you have a hundred people per ship,

  • that's 10,000 trips. So I think at least

  • a hundred people per trip is the right

  • order of magnitude, and I think we may

  • actually end up expanding the crew

  • section and ultimately taking more like

  • 200 or more people per flight in order

  • to reduce the cost per person.

  • But it's -- you know

  • 10,000 flights is a lot of flights. So

  • you really want ultimately on the order

  • of a thousand ships. It will take a

  • while to build up to a thousand ships.

  • And so I think if you say, When would we

  • reach that million-person threshold?

  • From the point at which the first ship

  • goes to Mars, it's probably somewhere

  • between 20 to 50 total Mars rendezvous.

  • So it's probably somewhere between maybe

  • 40 to 100 years to achieve a fully

  • self-sustaining civilization on Mars.

  • So that's sort of the cross-section of

  • the ship. In some way, it's not that

  • complicated, really. It's made primarily

  • of an advanced carbon fiber. The carbon

  • fiber part is tricky when dealing with

  • deep cryogens and trying to achieve both

  • liquid and gas impermeability and not

  • have gaps occur due to cracking or

  • pressurization that would make the

  • carbon fiber leaky.

  • So this is a fairly significant

  • technical challenge, to make deep and

  • cryogenic tanks out of carbon fiber. And

  • it's only recently that we think the

  • carbon fiber technology has gotten to

  • the point where we can actually do this

  • without having to create a liner, some

  • sort of metal liner, quad liner on the

  • inside of the tanks, which would add

  • mass and complexity.

  • It's particularly tricky for the hot

  • gaseous oxygen pressurization.

  • So this is designed to be autogenously

  • pressurized, which means that the fuel

  • and the oxygen, we gasify them through

  • heat exchanges in the engine and use

  • that to pressurize the tanks. So we will

  • gasify the methane and use that to

  • pressurize the fuel tank. Gasify the

  • oxygen. Use that to pressurize the

  • oxygen tank.

  • This is a much simpler system than what

  • we have with Falcon 9, where we use

  • helium for pressurization and we use

  • nitrogen for gas thrusters. In this

  • case, we would autogenously pressurize

  • and then use gaseous methane and oxygen

  • for the control thrusters.

  • So really, you only need two ingredients

  • for this, as opposed to four in the case

  • of Falcon 9 and actually five if you

  • consider the ignition liquid. It's sort

  • of a complicated liquid to ignite the

  • engines.

  • That isn't very usable. In this case we

  • would use spark ignition.

  • So this gives you a sense of vehicles by

  • performance, sort of current and

  • historic. I don't know if you can

  • actually read that. But in expandable

  • mode, the vehicle, of course, we are

  • proposing would do about 550 tons and

  • about 300 tons in reusable mode. That

  • compares to satisfy max capability of

  • 135 tons. But I think this really gives

  • a better sense of things.

  • The white bars show the performance of

  • the vehicle; in other words, the

  • payload-to-orbit of the vehicle. So you

  • can see essentially what it represents

  • is what's the size efficiency of the

  • vehicle. And most rockets, including

  • ours -- ours as they're currently flying

  • -- the performance bar is only a small

  • percentage of the actual size of the

  • rocket.

  • But with the interplanetary system which

  • we will initially use for Mars, we've

  • been able to -- or we believe massively

  • improve the design performance. So it's

  • the first time a rocket's sort of

  • performance bar will actually exceed the

  • physical size of the rocket.

  • This gives you a more direct sort of

  • comparison. This is -- the thrust that

  • is quite enormous, talking about liftoff

  • thrusts of 13,000 tons. So it's quite

  • tectonic when it takes off. But it is --

  • it is a fit on Pad 39A, which NASA has

  • been kind enough to allow us to use,

  • where -- because they somewhat oversized

  • the pad in doing Saturn 5 and, as a

  • result, we can actually do a much larger

  • vehicle on that same launch pad. And in

  • the future, we expect to add additional

  • launch locations, probably adding one on

  • the south coast of Texas.

  • But this gives you a sense of the

  • relative capability, if you can read

  • those.

  • But these vehicles have very different

  • purposes. This is really intended to

  • carry huge numbers of people, ultimately

  • millions of tons of cargo to Mars. So

  • you really need something quite large in

  • order to do that.

  • So talk about some of the key elements

  • of the interplanetary spaceship and

  • rocket booster. We decided to start off

  • the development with what we think are

  • probably the two most difficult elements

  • of the design. One is the Raptor engine.

  • And this is going to be the highest

  • chamber pressure engine of any kind ever

  • built and probably the highest

  • thrust-to-weight.

  • It's a full-flow staged combustion

  • engine which maximizes the theoretical

  • momentum that you can get out of a given

  • source fuel and oxidizer. We subcool the

  • oxygen and methane to densify it. So

  • compared to when -- propellants normally

  • use close to their boiling point in most

  • rockets. In our case, we actually build

  • the propellants close to their freezing

  • point. That can result in a density

  • improvement of up to around 10 to 12%,

  • which makes an enormous difference in

  • the actual results of the rocket. It

  • also makes the -- it gets rid of any

  • cavitation risk for the turbo pumps and

  • it makes it easier to feed a

  • high-pressure turbo pump if you have

  • very cold propellant.

  • Really one of the keys here, though, is

  • the vacuum version of Raptor having a

  • 382-second ISP. This is really quite

  • critical too to the whole Mars mission.

  • And we can get to that number or at

  • least within a few seconds of that

  • number, ultimately maybe exceeding it

  • slightly.

  • So the rocket booster in many ways is

  • really a scaled-up version of the Falcon

  • 9 booster. You will see a lot of

  • similarities, such as the grid fins.

  • Obviously clustering a lot of engines at

  • the base. And the big difference really

  • being that the primary structure is an

  • advanced form of carbon fiber as opposed

  • to limited lithium and that we use

  • autogenous pressurization and get rid of

  • the helium and the nitrogen.

  • So this uses 42 Raptor engines. It's a

  • lot of engines, but we use an I.N. on

  • the Falcon 9. And with Falcon Heavy,

  • which should launch early next year,

  • there's 27 engines on the base. So we've

  • got pretty good experience with having a

  • large number of engines. It also gives

  • us redundancies. So that if some of the

  • engines fail, you can still continue the

  • mission and be fine.

  • But the main job of the booster is to

  • accelerate the spaceship to around 8 1/2

  • thousand kilometers an hour. For those

  • that are less familiar with orbital

  • dynamics, really it's all about velocity

  • and not about height. So really that's

  • the job of the booster. The booster is

  • like the javelin thrower. You've got to

  • toss that javelin, which is the

  • spaceship.

  • In the case of other planets, though,

  • which have a gravity well which is not

  • as deep, so Mars, the moons of Jupiter,

  • conceivably maybe even one day Venus --

  • the -- well, Venus will be a little

  • trickier. But for most of the solar

  • system, you only need the spaceship. So

  • you don't need the booster if you have a

  • lower gravity well. No booster is needed

  • on the moon or Mars or any of the moons

  • of Jupiter or Pluto. You just need the

  • spaceship. The booster is just there for

  • heavy gravity wells.

  • And then we've also been able to

  • optimize the propellant needed for

  • boost-back and landing to get it down to

  • about 7% of the liftoff prop propellant

  • load. We think with some optimization

  • maybe we can get it down to about 6%.

  • And we also are now getting quite

  • comfortable with the accuracy of the

  • landing. If you have been watching the

  • Falcon 9 landings, you will see that

  • they are getting increasingly closer too

  • to the bull's-eye. And we think,

  • particularly with the addition of

  • additional -- with the addition of some

  • thrusters and maneuvering thrusters, we

  • can actually put the booster right back

  • on the launch stand. And then those fins

  • at the base are essentially centering

  • features to take out any minor position

  • mismatch at the launch site.

  • So that's what it looks like at the

  • base. So we think we only need to gimbal

  • or steer the center cluster of engines.

  • There's seven engines in the center

  • cluster. Those would be the ones that

  • move for steering the rocket, and the

  • other ones would be fixed in position,

  • which gives us the best concentration of

  • -- we can max out the number of engines

  • because we don't have to leave any room

  • for gimbaling or moving the engines.

  • And, like, this is all designed so that

  • you could actually lose multiple engines

  • even at liftoff or anywhere in flight

  • and continue the mission safely.

  • So for the spaceship itself, in the top,

  • we have the pressurized compartment. And

  • I'll show you a fly-through of that in a

  • moment. And then beneath that is the --

  • is where we would have the unpressurized

  • cargo, which would be really flat packed

  • in a very dense format.

  • And then below that is the liquid oxygen

  • tank. The liquid oxygen tank is probably

  • the hardest piece of this whole vehicle

  • because it's got to handle propellant at

  • the coldest level and the tanks

  • themselves actually form the air frame.

  • So the air frame structure and the tank

  • structure are combined, as it is in all

  • modern rockets. And in aircraft, for

  • example, the wing is really a fuel tank

  • in wing shape. So it has to take the

  • thrust loads of ascents, the loads of

  • reentry, and then it has to be

  • impermeable to gaseous oxygen, which is

  • tricky, and non-reactive to gaseous

  • oxygen. So that's the hardest piece of

  • the spaceship itself, which is actually

  • why we started on that element as well.

  • And I'll show you some pictures of that

  • later.

  • And then below the oxygen tank is the

  • fuel tank, and then the engines are

  • mounted directly to the thrust cone on

  • the base. And then there are six of the

  • vacuum -- the high efficiency vacuum

  • engines around the perimeter, and those

  • don't gimbal. And then there are three

  • of the sea-level versions of the engine

  • which do gimbal and provide the

  • steering. Although we can do some amount

  • of steering if you're in space with

  • differential thrust on the outside

  • engines.

  • The net effect is a cargo to Mars of up

  • to 450 tons, depending upon how many

  • refills you do with the tanker. And the

  • goal is at least 100 passengers per

  • ship. Although I think we will see that

  • number grow to 200 or more.

  • This chart is a little difficult to

  • interpret at first, but we decided to

  • put it there for people who wanted to

  • watch the video afterwards and sort of

  • take a closer look and analyze some of

  • the numbers.

  • The column on the left is probably

  • what's most relevant. And that gives you

  • the trip time. So depending upon which

  • Earth-Mars rendezvous you are aiming

  • for, the trip time at 6 kilometers per

  • second departure blast speed can be as

  • low as 80 days. And then over time, I

  • think we could probably improve that.

  • Ultimately, I suspect that you would see

  • Mars transit times of as little as 30

  • days in the more distant future.

  • It's fairly manageable, considering the

  • trips that people used to do in the old

  • days would routinely take sailing

  • voyages that would be six months or

  • more.

  • So on arrival, the heat shield

  • technology is extremely important. We

  • have been refining the heat shield

  • technology using our Dragon spacecraft.

  • We are now on version 3 of PICA, which

  • is the phenolic-impregnated carbon

  • ablator. And it's getting more and more

  • robust with each new version, with less

  • ablation, more resistance, less need for

  • refurbishment.

  • The heat shield is basically a giant

  • brake pad. How it's like how good can

  • you make that brake pad against the

  • extreme conditions and the cost of

  • refurbishment and make it so you could

  • have many flights with no refurbishment

  • at all.

  • This is a fly-through of the crew

  • compartment.

  • I just want to give you a sense of what

  • it would feel like to actually be in the

  • spaceship. I mean, in order to make it

  • appealing and increase that portion of

  • the Venn diagram of people who actually

  • want to go, it's got to be really fun

  • and exciting, and it can't feel cramped

  • or boring. But the crew compartment or

  • the occupant compartment is set up so

  • you can do zero-G things, you can float

  • around. It would be like movies,

  • ElectroPuls, cabins, a restaurant. It

  • will be, like, really fun to go. You are

  • going to have a great time.

  • (Laughter).

  • So the propellant plant on Mars, again,

  • this is one of those slides that I won't

  • go into in detail here, but people can

  • take that offline. The key point being

  • that the ingredients are there on Mars

  • to create a propellant plant with

  • relative ease, because the atmosphere is

  • primarily CO2 and there's water ice

  • almost everywhere. You've got the CO2

  • plus H2O to make methane CH4 and oxygen

  • O2 using the Sabatier reaction. The

  • trickiest thing really is the energy

  • source, which think we can do with a

  • large field of solar panels.

  • So then to give you a sense of the cost,

  • really the key is making this affordable

  • to almost anyone who wants to go. And we

  • think, based on this architecture, this

  • architecture, assuming optimization over

  • time, like the very first flights would

  • be fairly expensive. But the

  • architecture allows for a cost per

  • ticket of less than $200,000, maybe as

  • less -- maybe as little as $100,000 over

  • time, depending upon how much mass a

  • person takes. So we're right now

  • estimating about $140,000 per ton to the

  • trips to Mars. So if a person plus their

  • luggage is less than that, take into

  • account food consumption and life

  • support, then we think that the cost of

  • moving to Mars ultimately could drop

  • below $100,000.

  • So funding, talking about funding

  • sources. So we have steel underpants;

  • launch satellites; send cargo to space

  • station; Kickstarter, of course;

  • followed by profit. So obviously it's

  • going to be a challenge to fund this

  • whole endeavor. We do expect to generate

  • pretty decent net cash flow from

  • launching lots of satellites and serving

  • the space station for NASA, transferring

  • cargo to and from space station, and

  • then I know there's a lot of people in

  • the private sector who are interested in

  • helping fund a base on Mars and then

  • perhaps there will be interest on the

  • government sector side to also do that.

  • Ultimately, this is going to be a huge

  • public-private partnership. And I think

  • that's -- that's how the United States

  • was established, and many other

  • countries around the world, is a

  • public-private partnership. So I think

  • that's probably what occurs.

  • And right now we're just trying to make

  • as much progress as we can with the

  • resources that we have available and

  • just sort of keep moving both forward.

  • And, hopefully, I think as we -- as we

  • show that this is possible, that this

  • dream is real, not just a dream, it is

  • something that can be made real, I think

  • the support will snowball over time.

  • And I should say also the main reason

  • I'm personally accumulating assets is in

  • order to fund this. So I really don't

  • have any other motivation for personally

  • accumulating assets except to be able to

  • make the biggest contribution I can to

  • making life multiplanetary.

  • [APPLAUSE].

  • Time lines. Not the best at this sort of

  • thing. But just to show you where we

  • started off. In 2002, SpaceX basically

  • consisted of carpet and a mariachi band.

  • That was it. That's all of SpaceX in

  • 2002. As you can see, I'm a dancing

  • machine. And, yeah, I believe in kicking

  • off celebratory events with mariachi

  • bands. I really like mariachi bands.

  • But that was what we started off with in

  • 2002. And really, I mean, I thought we

  • had maybe a 10% chance of doing

  • anything, of even getting a rocket to

  • orbit, let alone getting beyond that and

  • taking Mars seriously. But I came to the

  • conclusion if there wasn't some new

  • entrant into the space arena with a

  • strong ideological motivation, then it

  • didn't seem like we were on a trajectory

  • to ever be a space-faring civilization

  • and be out there among the stars.

  • Because, you know, in '69 we were able

  • to go to the moon and the space shuttle

  • could get to low-Earth orbit, and then

  • after the space shuttle got retired. But

  • that trend line is down to zero.

  • So I think what a lot of people don't

  • appreciate is that technology does not

  • automatically improve. It only improves

  • if a lot of really strong engineering

  • talent is applied to the problem that it

  • improves. And there are many examples in

  • history where civilizations have reached

  • a certain technology level and then have

  • fallen well below that and then

  • recovered only millennia later.

  • So we go from 2002 where we're basically

  • -- we're clueless. And then with Falcon

  • 1, the smallest useful little rocket

  • that we could think of which would

  • deliver a half a ton to orbit, and then

  • four years later we developed the -- we

  • built the first vehicle. So we dropped

  • the main engine, the upper stage engine,

  • the air frames, the fairing and the

  • launch system and had our first attempt

  • at launch in 2006, which failed. So that

  • lasted about 60 seconds, unfortunately.

  • But it's 2006, four years after

  • starting, is also when we actually got

  • our first NASA contract. And I just want

  • to say I'm incredibly grateful to NASA

  • for supporting SpaceX, you know, despite

  • the fact that our rocket crashed. Of

  • course, I'm NASA's biggest fan. So, you

  • know, thank you very much to the people

  • that had the faith to do that. Thank

  • you.

  • [APPLAUSE].

  • So then 2006, followed by a lot of

  • grief. And then, finally, the fourth

  • launch of Falcon 1 worked in 2008. And

  • we were really down to our last pennies.

  • In fact, I only thought I had enough

  • money for three launches and the first

  • three bloody failed. And we were able to

  • scrape together enough to just barely

  • make it and do a fourth launch. And

  • thank goodness that fourth launch

  • succeeded in 2008. That was a lot of

  • pain.

  • And then also at the end of 2008 is when

  • NASA awarded us the first major

  • operational contract, which was for

  • resupplying cargo to the space station

  • and bringing cargo back.

  • Then a couple years later we did the

  • first launch of Falcon 9, version 1. And

  • that had about a 10-ton-to-orbit

  • capability. So it was about 20 times the

  • capability of Falcon 1, and also was

  • assigned to carry our Dragon spacecraft.

  • Then 2010 is our first mission to the

  • space station. So we were able to finish

  • development of Dragon and dock with the

  • space station in 2010. so -- Sorry, 2010

  • is expendable Dragon -- expendable

  • Dragon. 2012 is when we delivered and

  • returned cargo from the space station.

  • 2013 is when we first started doing boat

  • take-off and landing tests. And then

  • 2014 is when we were able to have the

  • first orbital booster do a soft landing

  • in the ocean. The landing was soft. The

  • (inaudible) exploded. But the landing --

  • for seven seconds, it was good. And we

  • also improved the capability of the

  • vehicle from 10 tons to about 13 tons to

  • LEO.

  • And then 2015, last year, in December,

  • that was definitely one of the best

  • moments of my life when the rocket

  • booster came back and landed at Cape

  • Canaveral. That was really ...

  • [APPLAUSE].

  • Yeah. So that really showed that we

  • could bring an orbit-class booster back

  • from a very high velocity all the way to

  • the launch site and land it safely and

  • with almost no refurbishment required

  • for reflight. And if things go well,

  • we're hoping to refly one of the landed

  • boosters in a few months.

  • So, yeah -- and then 2016, we also

  • demonstrate landing on a ship. The

  • landing on the ship is important for the

  • very high-velocity geosynchronous

  • missions. And that's important for

  • reusability of Falcon 9 because about

  • roughly a quarter of our missions are

  • sort of servicing the space station. But

  • then there's a few other low-Earth-orbit

  • missions. But most of our missions,

  • probably 60% of our missions, are

  • commercial geo missions. So we've got to

  • do these high-velocity missions that

  • really need to land on a ship out to

  • sea. They don't have enough propellants

  • on board to boost back to the launch

  • site.

  • So looking into the future, next steps,

  • we were kind of intentionally a bit

  • fuzzy about this time line. But we were

  • going to try to make as much progress as

  • we can. Obviously, it's with a very

  • constrained budget. But we are going to

  • try to make as much progress as we can

  • on the elements of interplanetary

  • transport booster and spaceship, and

  • hopefully we'll be able to complete the

  • first development spaceship in maybe

  • about four years and start doing

  • suborbital flights with that.

  • In fact, it has enough capability that

  • you could maybe even go to orbit if you

  • limit the amount of cargo with the

  • spaceship. Well, you have to really --

  • you have to really strip it down. But in

  • tanker form, it could definitely get to

  • orbit. It can't get back, but it can get

  • to orbit.

  • Actually, I was thinking like maybe

  • there is some market for really fast

  • transport of stuff around the world,

  • provided we can land somewhere where

  • noise is not a super big deal, because

  • rockets are very noisy. But we could

  • transport cargo to anywhere on Earth in

  • 45 minutes at the longest. So most

  • places on Earth would be maybe 20, 25

  • minutes. So maybe if we had a floating

  • platform off the coast of, you know, say

  • -- off the coast of New York, say 20, 30

  • miles out, could you go from New York to

  • Tokyo in, I don't know, 25 minutes;

  • across the Atlantic in ten minutes.

  • Really most of your time would be

  • getting to the ship, and then it would

  • be real quick after that.

  • So there's some intriguing possibilities

  • there. Although, we're not counting on

  • that.

  • And then development of the booster --

  • we actually think the booster part is

  • relatively straightforward because it's

  • -- it amounts to a scaling up of the

  • Falcon 9 booster. So there's -- we don't

  • see a lot of sort of show-stoppers

  • there. Yeah.

  • But then trying to put it all together

  • and make this actually work to Mars, if

  • things go super well, it might be kind

  • of in the ten-year time frame. But I

  • don't want to say that's when it will

  • occur. It's, like, this huge amount of

  • risk. It's going to cost a lot. Good

  • chance we don't succeed, but we're going

  • to do our best and try to make as much

  • progress as possible.

  • And we're going to try to send something

  • to Mars on every Mars rendezvous from

  • here on out. So Dragon 2, which is a

  • propulsive lander, we plan to send to

  • Mars in a couple years, and then do

  • probably another Dragon mission in 2020.

  • In fact, we want to establish a steady

  • cadence, that there's always a flight

  • leaving, like there's a train leaving

  • the station. With every Mars rendezvous

  • we will be sending a Dragon -- at least

  • a Dragon to Mars and ultimately the big

  • spaceship.

  • So if there's a lot of interest in

  • putting payloads on Dragon, you know you

  • can count on a ship that's going to

  • transport something on the order of at

  • least two or three tons of useful

  • payloads to the surface of Mars.

  • [APPLAUSE].

  • That's part of the reason we designed

  • Dragon 2, to be a propulsive lander. As

  • a propulsive lander, you can go anywhere

  • in the solar system. So you can go to

  • the moon. You can go to -- well,

  • anywhere, really. Whereas, if something

  • relies on parachutes or wings, then you

  • can pretty much only -- well, if it's

  • wings, you can pretty much only land on

  • Earth because you need a runway, and

  • most places don't have a runway. And

  • then anyplace that doesn't have a dense

  • atmosphere, you can't use parachutes.

  • But propulsive works anywhere. So the

  • Dragon should be capable of landing on

  • any solid or liquid surface in the solar

  • system.

  • I was real excited to see that the team

  • managed to do the -- all our Raptor

  • engine firing in advance of this

  • conference. I just want to say thanks to

  • the Raptor team for really working seven

  • days a week to try to get this done in

  • advance of the presentation, because I

  • really wanted to show that we've made

  • some hardware progress in this

  • direction. And the Raptor is a really

  • tricky engine. It's a lot trickier than

  • Merlin because it's a full-flow stage

  • combustion, much higher pressure.

  • I'm kind of amazed it didn't blow up on

  • the first firing. Fortunately, it was

  • good.

  • It's kind of interesting to see the mock

  • diamonds forming.

  • [APPLAUSE].

  • And part of the reason for making the

  • engine sort of small, Raptor, although

  • it has three times the thrust of a

  • Merlin is only about the same size as a

  • Merlin engine because it has three times

  • the operating pressure.

  • That means we can use a lot of the

  • production techniques that we've honed

  • with Merlin.

  • We are currently producing Merlin

  • engines at almost 300 per year. So we

  • understand how to make rocket engines in

  • volume.

  • Even though the Mars vehicle uses 32 on

  • the base and 9 on the upper stage, so we

  • are at 51 engines to make -- that's well

  • within our production capabilities for

  • Merlin. And this is a similarly sized

  • engine to Merlin except for the

  • expansion ratio. So we feel really

  • comfortable about being able to make

  • this engine in volume at a price that

  • doesn't break our budget.

  • We also wanted to make progress on the

  • primary structure. So, as I mentioned,

  • this is really a very difficult thing to

  • make, to make something out of carbon

  • fiber.

  • Even though carbon fiber has incredible

  • strength-to-weight, when you want to

  • then put super cold liquid oxygen or

  • liquid methane -- particularly liquid

  • oxygen -- in a tank, it's subject to

  • cracking and leaking, and it's very

  • difficult to make. Just the sheer scale

  • of it is also challenging, because

  • you've got to lay out the carbon fiber

  • in exactly the right way on a huge mold,

  • and you've got to cure that mold at

  • temperature.

  • And then -- it's just hard to make large

  • carbon fiber structures that could do

  • all of those things and carry incredible

  • loads. So that's the other thing we want

  • to focus on is the Raptor and then

  • building the first development tank for

  • the Mars spaceship.

  • So this is really the hardest part of

  • the spaceship. The other pieces we have

  • a pretty good handle on. But this was

  • the trickiest one. We wanted to tackle

  • it first.

  • You get a size for how big the tank is,

  • which is really quite big. Also big

  • congratulations to the team that worked

  • on that.

  • They were also working seven days a week

  • to try to get this done in advance of

  • the IAC. We managed to build the first

  • tank, and the initial tests with the

  • cryogenic propellants actually look

  • quite positive. We have not seen any

  • leaks or major issues.

  • This is what the tank looks like on the

  • inside. So you can get a real sense for

  • just how big this tank is. It's actually

  • completely smooth on the inside, but the

  • way that the carbon fiber plies lay out

  • and reflect the light makes it look

  • faceted.

  • So then what about beyond Mars?

  • So as we thought about the system -- and

  • the reason we call it a system, because

  • generally I don't like calling things

  • systems because everything is a system,

  • including your dog -- is that -- is that

  • it's actually more than a vehicle.

  • There's obviously the rocket booster,

  • the spaceship, the tanker, and the

  • propellant plant, the in situ propellant

  • production.

  • If you have all of those four elements,

  • you can actually go anywhere in the

  • solar system by planet hopping or moon

  • hopping. So by establishing a propellant

  • depot on -- in the asteroid belt or on

  • one of the moons of Jupiter, you can go

  • to -- you can make flights from Mars to

  • Jupiter no problem. In fact, even from

  • -- even without a propellant depot at

  • Mars, you can do a fly-by of Jupiter

  • without a propellant depot.

  • So -- but by establishing a propellant

  • depot, let's say, you know, Enceladus or

  • Europa or -- there's a few options, and

  • then doing another one on Titan,

  • Saturn's moon, and then perhaps another

  • one further out on Pluto or elsewhere in

  • the solar system, this system really

  • gives you freedom to go anywhere you

  • want in the greater solar system. So you

  • can actually travel out to the Kuiper

  • belt or the Earth cloud. I wouldn't

  • recommend this for interstellar

  • journeys, but this -- just this basic

  • system, provided we have filling

  • stations along the way, is -- means full

  • access to the entire greater solar

  • system.

  • [APPLAUSE].

JEAN LEGALL: Good afternoon, ladies and

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