Author Topic: Elon Musk IAC Mars Speech - Sept. 27, 2016 - DISCUSSION THREAD  (Read 441707 times)

Offline Rocket Science

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I haven't read all the comments in this thread. But I sort of wonder what is the best way to describe the spacecraft, it seems like a cross between a capsule and a lifting body. It has a black heatshield on one side.

Yes, it seems to me to be a new class of spaceflight vehicle:  it is a sort of integrated second-stage and spacecraft rolled into one.  Not something we've seen much of (if any) before.

The on-orbit re-propellanting for the BEO missions allows the spacecraft itself to also fulfill the role that a second stage usually fulfills in the LV design.

This is the first true Spaceship.  Apollo and all previous spacecraft were payloads.
I'd argue the the LEM was first...
"The laws of physics are unforgiving"
~Rob: Physics instructor, Aviator

Offline savuporo

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- What magic will keep both propellant in tanks for several months
- Spark ignited, strung out turbopumped deep space propulsion ? What kind of redundancy and whats the testing regime for this ?

Radiators, narrow aspect to the sun(engines toward the sun), cryo-coolers... some combination of these low grade technologies.
Can you point to these things on these diagrams supposedly made from CAD models ? How big are these solar arrays to run everything, again, at Martian solar flux ?

Quote
Testing in Cis-Lunar space -- the proving ground.
I thought SpaceX isn't going anywhere near the Moon ? Did you just make that up or is there any cite or reference for this ?

Solar powered liquefaction pumps that take boil off and re-condense? Maybe just some sub cooling so there is no boil off. refrigerators are easy.
Refrigeration in space is easy ? ISS ammonia loops disagree


Edit/Lar: "Considering the overall thrust and Delta-BS required, these threads are running way too snark-lean anyway" No they aren't. NSF is not a place for snark.
« Last Edit: 09/28/2016 05:22 pm by Lar »
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Offline meekGee

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It sounds like its the actual tank for the initial ship that they plan on using for testing.
I'm wondering where they will test it. Hawthorne factory probably not best place for exprerimental LOX tank. Could they transport something that big to more safe place?

Also landing legs don't like sturdy enough to hold fully fueled spaceship, even on mars.

Do we know this tank is in hawthorne?

Where are the toolings for it?  It could not have been transported in by road.

Maybe SpaceX has another facility somewhere?
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Offline jpo234

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- What magic will keep both propellant in tanks for several months

Look at the schematics on slide 26: there are smaller tanks inside the main tanks.
They need gases for pressurization. Etc.

No, they don't. Once again slide 26: "Autogenous pressurization".
You want to be inspired by things. You want to wake up in the morning and think the future is going to be great. That's what being a spacefaring civilization is all about. It's about believing in the future and believing the future will be better than the past. And I can't think of anything more exciting than being out there among the stars.

Offline Rocket Science

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I was disappointed. Musk seems to subscribe to the idea that space colonization (of whatever sort) is basically a transportation problem and his presentation was virtually all about transportation. I think that kind of narrow focus is a huge mistake which will become more obvious as time goes on.

Maybe. I think transportation is his first priority. The overall planning of how a Mars colony could develop is critical, and he must have outlines of how it can come together, problems to be overcome etc, because private enterprise and the competitive aspect he wants needs a structure to build from.

But he is hoping for collaboration. And he may plan on handing that over to another company. Perhaps MarsX, but he may hope for NASA too.

So a reason to not say much about it?
EM's analogy to the Union-Pacific seems spot-on. He's trying to make it possible for other companies to risk their assets, and for individuals to commit part of their lives, for the opportunity to start a grand adventure.

It's been over 50 years since I learned about that railroad in school (so feel free to correct my version of history), but it and the later ones were heavily subsidized by the federal government - the railroad companies were outright given all of the land on either side of the right-of-way, out to 50 miles. Initially there was nothing between the endpoints. However, this was coincident with arrival of huge numbers of immigrants to the US, and lots of them took the chance to move into the wilderness and farm that same land. The crops produced had to be shipped out, which increased the justification for the railroad. Et cetera. More people, more economic activity, more innovation, gradually less rugged conditions. Took a long time, but now we have all of those excellent cities, roads, businesses, and farms.

But none of that would have happened if the railroad hadn't been built. So yeah, EM is pushing a transportation system. I would be surprised if his people haven't been working on solutions to all of these other problems, too, but making it practical to get there is positively Job #1.
IIRC those railroad companies got subsidies and grants and the nation benefited by having a transcontinental RR to transport it's citizens and moving goods to markets. Where in the nation's benefit in dong this for Mars?

You cannot think of a benefit from an American company developing a Mars Transportation System that can put people and cargo on another planet for peanuts?
Fine for a company from any country, sure... It has to benefit "all" the average US citizens/taxpayers in a government role...
"The laws of physics are unforgiving"
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Offline Jim Davis

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You cannot think of a benefit from an American company developing a Mars Transportation System that can put people and cargo on another planet for peanuts?

It all hinges on the question of whether Mars is a planet on which people can live and thrive. Musk didn't address that question; he assumes that that is the case, as do most people on this forum.

If I rephrase your question to read:

"You cannot think of a benefit from an American company developing a Transportation System that can put people and cargo in the interior of Greenland for peanuts?"

The answer is obvious. No, I can't think of the benefits.

Again, it all comes down to whether people can live and thrive on Mars. At this point it's an article of faith that they can. I was hoping Musk would move the matter beyond that point. I was disappointed.

Offline Cherokee43v6

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I was disappointed. Musk seems to subscribe to the idea that space colonization (of whatever sort) is basically a transportation problem and his presentation was virtually all about transportation. I think that kind of narrow focus is a huge mistake which will become more obvious as time goes on.

Maybe. I think transportation is his first priority. The overall planning of how a Mars colony could develop is critical, and he must have outlines of how it can come together, problems to be overcome etc, because private enterprise and the competitive aspect he wants needs a structure to build from.

But he is hoping for collaboration. And he may plan on handing that over to another company. Perhaps MarsX, but he may hope for NASA too.

So a reason to not say much about it?
EM's analogy to the Union-Pacific seems spot-on. He's trying to make it possible for other companies to risk their assets, and for individuals to commit part of their lives, for the opportunity to start a grand adventure.

It's been over 50 years since I learned about that railroad in school (so feel free to correct my version of history), but it and the later ones were heavily subsidized by the federal government - the railroad companies were outright given all of the land on either side of the right-of-way, out to 50 miles. Initially there was nothing between the endpoints. However, this was coincident with arrival of huge numbers of immigrants to the US, and lots of them took the chance to move into the wilderness and farm that same land. The crops produced had to be shipped out, which increased the justification for the railroad. Et cetera. More people, more economic activity, more innovation, gradually less rugged conditions. Took a long time, but now we have all of those excellent cities, roads, businesses, and farms.

But none of that would have happened if the railroad hadn't been built. So yeah, EM is pushing a transportation system. I would be surprised if his people haven't been working on solutions to all of these other problems, too, but making it practical to get there is positively Job #1.
IIRC those railroad companies got subsidies and grants and the nation benefited by having a transcontinental RR to transport it's citizens and moving goods to markets. Where in the nation's benefit in dong this for Mars?

You cannot think of a benefit from an American company developing a Mars Transportation System that can put people and cargo on another planet for peanuts?
Fine for a company from any country, sure... It has to benefit "all" the average US citizens/taxpayers in a government role...

No, it doesn't have to benefit 'all'.  Just a large (and loud) enough minority to make the congresscritters think it does.

If half the laws passed and programs paid for in the last 50 years were held to that criteria, then none of them would have been done.
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Offline MP99

Considering the new booster is a really massive rocket and it will have to make hundreds if not thousands of launches, that is a significant environmental impact from a greenhouse gas emission point of view.

In the following decades politics and population will become increasingly sensitive to that as climate change effects start affecting the living quality of the western world general population to a higher degree.

As Elon Musk has said in the past, Rockets are unfortunately the only thing that can not be run electrically.

Except they can:

SpaceX already needs to develop large scale In Situ propellant synthesis from water and carbon dioxide for the mars operation. All it needs is CO2 + H2O + Energy.

These elements are as readily available on Earth. Building a large propellant synthesis plant in combination with regenerative energy sources near the launch pad will solve two issues at once:

ITS will fly "green" with a 0 net carbon footprint
The In Situ technology can have a large scale test run on earth to see if there's any issues with long term operation and upscaling. (On Mars it'd be a bit late if some critical catalyst starts to degrade over time ad you have no spares)

Some marketing dude will point out that this scheme removes CO2 from the atmosphere, and dumps some of it on Mars, which will make it "better than 0 net".

Unfortunately, most of the expended propellant will fall back into the atmosphere, AFAICT, so more of a marketing thing than a genuine contribution to the problem.

Cheers, Martin

Offline Semmel

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There are several unique features of the BFR/ICT that are unheard of today. Some of them game changing, some of them simply different than anybody else. I try to catch them all:

1. Full Flow Staged Combustion engine. First engine of its kind in production if it makes it. Also, highest chamber pressure of any liquid fuel engine. Together maybe the technologically most advanced engine in the world, arguably the best engine.

2. All carbon composite tanks. Never done before on a rocket.

3. "Autogenous pressurization", especially for LOX is unheard of in modern rockets. The corrosive properties of hot gaseous oxygen must be a nightmare to tame. Not to mention the fact that everything tends to go up in flames in pure and hot oxygen atmospheres.

4. Only 2 liquids, no nitrogen, no hypergolics, no helium. This came as a requirement from Mars because these things are very hard to produce on Mars. Still, no modern rocket is that limited in its liquids/gases. Not sure if this is good or bad compared to other rockets. Specifically, it means that altitude thrusters are fed from the main fuel tank, never done before as far as I know. (BTW, nobody seems to notice so far that this requires a new type of altitude thruster engine from SpaceX)

5. Cryogenic fuel storage for month at a time in space and refueling in orbit. Not magic but never done before to increase delivered payload.

6. Fully reusable system. If it is low-maintenance, it becomes what the Shuttle promised but never delivered with similar development cost but 10 times more payload. Also, booster land on launch pad. Seems crazy at the moment.

7. Private company designs a rocket that has not to the goal of generating revenue. Cant remember that I ever heard that one before. Its more like a state owned company that has national security aspects in mind rather than revenue. Financially, sounds crazy to me. Ideologically, absolutely makes sense, like scifi loosing the "fi" part.

Offline Nibb31

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Do we have any hard data that the Tankers would definitely have/use legs?

If landing on a cradle is modus operandi for the Booster, then perhaps is also for the Tankers.  In which case, leave off the legs, and carry more propellant.

Do you really think the booster will be designed to survive the thrust of 3 raptor engines landing on top of it?

Offline robert_d

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Also landing legs don't like sturdy enough to hold fully fueled spaceship, even on mars.

Maybe they could roll additional support under or gently lift the empty Spaceship, put wheels underneath the legs and roll it to a prepared launch site with support and flame trench.



Offline rsdavis9

- What magic will keep both propellant in tanks for several months

Look at the schematics on slide 26: there are smaller tanks inside the main tanks.
They need gases for pressurization. Etc.

No, they don't. Once again slide 26: "Autogenous pressurization".
Autogenous pressurization works because gaseous o2(from the engine) is fed back into the lox tank and gaseous ch4 is fed back into the liquid ch4 tank.  So there is gases for pressurization. I argue they may need to store some of the gas to use at a latter time when the engines are not running.

What do you think is in the spherical tanks? I count one in each tank in the S2 and one in the methane tank in S1.
With ELV best efficiency was the paradigm. The new paradigm is reusable, good enough, and commonality of design.
Same engines. Design once. Same vehicle. Design once. Reusable. Build once.

Offline RonM

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Do we have any hard data that the Tankers would definitely have/use legs?

It's in the video.




Offline pobermanns

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Wowza. The ITS is one impressive rocket. 42 engines in the first stage. How many engines can fail and the rocket still get the Mars ship to a useful orbit? Elon said "multiple". I would expect each engine to be surrounded by shielding to prevent one Raptor RUD from taking out the others (like what happened with N-1?).

As far as the ITS crewed vessel, one question that occurs to me is how much payload would it carry if it were just being launched by itself (SSTO) into a low earth orbit like the one Shuttle used? Elon said it was a small number. Better yet, how much of a payload would it carry on a suborbital flight, say from New York to London? If they test it on suborbital hops and find it can work well I wouldn't be surprised if Elon tries to make money by pioneering transoceanic suborbital cargo & passenger services, after all he'll need lots of income to pull this off.

Speaking of tourism, if ITS really works and they fly people as far as Saturn I could see myself enjoying a tourist flight to see the rings of Saturn close up, if I make it out that far.....

Musk being the environmentalist that he is, would probably not use the ITS as a intercontinental cargo/people mover.  The carbon footprint would be astronomically higher than even the most fuel thirsty airplane.  Yes, your package would get to London in a matter of minutes,  but you're burning millions of pounds of methane doing so.
So, you're burning millions of pounds of one greenhouse gas (methane) and producing millions of pounds of a different greenhouse gas (CO2). Why is this a problem?

Offline dnavas

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How many flights do you need to be confident enough not to have an abort strategy?
How do you get that flight count on a brand new engine and launch system?
I guess you have to retire the risk on each system then the vehicle as a whole and Elon makes the call on what is acceptable since he is running his own space agency here. Now if you ask in light of the recent failures color me a bit skeptical at this point...

Well, I ask given that the answer seems to suggest that the Raptor needs another system to run in in order to "retire the risk" as you say.  You're right, of course, that the recent failures force me to set the bar a little higher than "trust SX", but the thrust of my point was to wonder what that other system is....


Offline savuporo

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There are several unique features of the BFR/ICT that are unheard of today. Some of them game changing, some of them simply different than anybody else. I try to catch them all:..
A few other missed aspects, but importantly, nobody has taken a pump fed engine beyond earth departure burns, i.e. just hours of loiter time at max, not months. Everything that has fired in space beyond that has been pressure-fed hypergolic ( or electric propulsion), with differing layers of redundancy in very simple engines.
The reliability of this will be interesting, to say the least.
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Offline mme

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...
Musk being the environmentalist that he is, would probably not use the ITS as a intercontinental cargo/people mover.  The carbon footprint would be astronomically higher than even the most fuel thirsty airplane.  Yes, your package would get to London in a matter of minutes,  but you're burning millions of pounds of methane doing so.
So, you're burning millions of pounds of one greenhouse gas (methane) and producing millions of pounds of a different greenhouse gas (CO2). Why is this a problem?
Unless you extracted the methane from the atmosphere you are still transferring previously "stored" carbon into the atmosphere.  If they use methane that was going to be released into the atmosphere or created the methane from carbon extracted from the atmosphere, that's a different matter.
Space is not Highlander.  There can, and will, be more than one.

Offline Ronsmytheiii

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Well, I ask given that the answer seems to suggest that the Raptor needs another system to run in in order to "retire the risk" as you say.  You're right, of course, that the recent failures force me to set the bar a little higher than "trust SX", but the thrust of my point was to wonder what that other system is....

Well Like Elon said the engine is the same physical size of the Merlin engine, and the USAF is paying them to develop an upperstage engine for Falcon through Raptor.....

Offline meekGee

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Do we have any hard data that the Tankers would definitely have/use legs?

It's in the video.



This video is like the reusability video.  It's a very good indication on where they're going, and it's the best source we have right now, but it's not infallible... 

It's sure more than an artists concept (as was the first one!) but don't use it as a bible.
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Offline Senex

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So, you're burning millions of pounds of one greenhouse gas (methane) and producing millions of pounds of a different greenhouse gas (CO2). Why is this a problem?

It's actually a lot better than a break even.   It's far better to burn methane than to let it get loose in the environment.  All those well flares are a good thing.

"While carbon dioxide is typically painted as the bad boy of greenhouse gases, methane is roughly 30 times more potent as a heat-trapping gas. " — Princeton University

https://blogs.princeton.edu/research/2014/03/26/a-more-potent-greenhouse-gas-than-co2-methane-emissions-will-leap-as-earth-warms-nature/




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