SpaceX Reveals Plans For Full Launch System Re-usability
FleaPlus writes "During a talk at the National Press Club, SpaceX's Elon Musk revealed the company's plans for making their Falcon 9 rocket fully reusable. A rendering depicts the first stage, upper stage, and Dragon capsule all separately returning to the Earth's surface and making a controlled, rocket-powered landing. During the next few years SpaceX will be testing VTVL (Vertical Takeoff, Vertical Landing) maneuvers and re-usability with their Falcon 9-based 'Grasshopper' testbed, with up to 70 test launches per year. Musk stated that if reuse is successful, it would result in a 100x reduction in their already-low launch costs, a key step toward Musk's long-term aim of lowering the price of a ticket to Mars to $500K."
I am glad Americans invested in the Space Shuttle programme that gave, among so many other benefits, the basic R&D into reusable space vehicles and launch systems for them, to SpaceX, the rest of the growing private space industry, and to the world in general.
I look forward to SpaceX and its competitors paying the taxes that will repay that investment, even as they make good profits without having had to take the risks or pay the costs of those decades of R&D on their own.
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make install -not war
Bizarrely, it's starting to feel like the old Flash Gordon / old cartoon style "rocket ships" are actually the future! I'm not sure I'll ever be able to see them as "retro" and less futuristic-looking than the shuttle, no matter how much more advanced and practical they actually are.
Commercially, without massive amounts of money spent on lobbying, and showing you can do it by generating significant results rather than shiny piles of paper that do not fly.
I note in the speech - at around 33 minutes - one telling quote.
(Paraphrasing, as it was yesterday I watched it) "We have 1% of the lobbying power of Boeing and Lockmart. If the decision depends on lobbying power, we're screwed'.
This was about the decision to extend the sole-source monopoly for airforce rockets.
And he notes also that the rationale to do this is to keep the industry alive. Engines for those rockets are built in russia, other parts in switzerland, whereas SpaceX builds all key subsystems themselves in the US.
500K ? Is that a return-ticket? Or one way?
That was a line from the backing song. Interesting choice.
On a different topic. It takes X amount of rocket fuel to move a payload to orbit. It takes Y amount of rocket fuel to soft land the components back to Earth. So can anyone give ball park figures for X and Y that would make sense in the context of delivering people to the ISS? It seems to me that scaling up X to include Y in the payload is a losing game.
I am Slashdot. Are you Slashdot as well?
No, I am truly in awe of this idea, if they pull off even a third of it they will roflstomp the national programs. As someone else commented, the music was an interesting choice, it really confers they are high confident of their design and eventuality of success. Frankly, stuff like this is what it will take to inspire the next generation about space because it is so fantastic looking.
* Winners compare their achievements to their goals, losers compare theirs to that of others.
This requires separate landing systems for each stage of the rocket. This is a lot more added mass. And the worst thing to add to a rocket is more mass. Simple reusable systems like parachutes (as were used by the shuttle's solid rocket boosters) are one thing, but full-out rocket powered landing will weigh a lot more, will require a lot of additional fuel, and will add all sorts of technical requirements.
At this point, it doesn't seem that chemical rockets will become that more efficient barring major breakthroughs, like much lighter alloys, or totally new chemical reactions for the fuel. Neither of these seem very likely right now, and the second seems to be much less likely. The first also won't do that much. At this point, I have to be wondering if we should be spending a lot more resources on researching non-rocket methods of going to space. It seems like we may have a bad example of technological lockin since we've put so much work into chemical rockets.
But there are a lot of other methods out there and we should be looking at them. Nuclear rockets are an obvious example, and they can be built without having any serious radioactivity (you use a conventional fission reactor to heat steam). The basic reactor can be suprisingly light- in the 1950s the US and the USSR both experimented with nuclear powered aircraft http://en.wikipedia.org/wiki/Nuclear_aircraft and reactor technology has improved a lot since then. Another possibility is a space gun. http://en.wikipedia.org/wiki/Space_gun. They have been successfully used to do suborbital lobs. They are completely reusable. And since they don't require sending most of their own fuel into space they avoid the common problem of needing more fuel to lift fuel (which is why rockets get bigger fast compared to the size of payload). There are more exotic ideas also like launch loops, space elevators, and space fountains but they seem to be much further from practicality at this point. In the case of space elevators, the main technical problem is making enough high quality nanotubes in a supporting resin, and research into that is ongoing because high quality carbon nanotubes will be useful a large number of different much more mundane technologies.
Wouldn't it be wise to include parachutes at some stage of the descent, to conserve some fuel?
Musk also confirmed that the currently scheduled November or December flight of SpaceX’s Dragon capsule to the space station will likely be delayed due to the failure of a Soyuz rocket carrying a Progress re-supply ship to the ISS on August 24, 2011.
“It actually will likely result in a delay to our launch to the ISS,” Musk said, “and NASA rightly wants to have the appropriate level of astronauts with the right training when we arrive, so it looks like January for the launch to space station, and that is contingent upon the Russians meeting the schedule they’ve currently stating."
It sounds reasonable, but it also sounds like someone doesn't want SpaceX to have the enormous PR gain of launching a mission to the ISS when everyone else's pants are down.
I peripherally worked on the DC-X program which was a single stage to orbit concept vehicle that would have eventually lead to a larger rocket that was considered as a shuttle replacement.
The problem with the DCX was that it had to reserve fuel for the landing. The whole idea was to take off from something no bigger than a heli-pad (no gantry, and just a few people manning launch control) fly, and land back on the heli-pad.
Worked great until you got to the landing part: Two big issues were during landing, thrust would bounce off the tarmac, and end up setting the rocket on fire, the other problem was the landing gear. On one test flight, one leg failed to deploy, the rocket landed, then tipped over and exploded... which essentially killed the project.
The DCX was conceived during Reagen's "Star Wars" project, and built and flown during the Clinton era.
Unless there's been some breakthrough for the Falcon, I believe Musk is going to run into exactly the same issues.
Personally, I believe Rutan is on a better track, following the X-15 and scaling up. That's the only method for full re-useability.
If telephones are outlawed, then only outlaws will have telephones.
I know it it has some merit, but I would think establishing a perm. moon base would be "what's next". Your only three or four days out, can work out the logistics, effects, communication, etc... See if people really do turn into jellyfish after 6 months in what 1/6 gravity. The only reason I can see for colonizing mars (at this point) is "because". Let's bet on black before we bet on green zero.
/-- So if could reuse it would lead to 100 times reduction in cost.
If they can (launch + re-assemble + launch) * 100 at no additional cost for repairs they need to let the engineers of the world know wtf they are making this rocket out of. I don't know of any substance or design that allows for that much use. These guys probably have private shark tanks with full laser gear so I'm not going to completely discount them. Regardless, the numbers sound way fishy.
Having to work for a living is the root of all evil.
And I'm revealing my plans for world domination with an army of supermodels.
SpaceX might want to do a little less revealing of plans and a little more flying in space. I'm getting tired of hearing about what they're gonna do and would like to hear a little more about what they've done besides send up another roman candle.
You are welcome on my lawn.
It's not just the fuel you need to soft land, but all of the other added components (heat shield, landing legs, incremental fuel tank size) to make up a "recovery system" that you need to consider. The fuel is the cheapest part of the formula. Against that incremental recovery system cost you have the savings of recovering the expensive parts of the rocket such as the engines. Since fuel tanks are relatively cheap compared to engines, on a per kg basis, it's worth spending a bit more on larger tanks to get the expensive engines back.
The actual numbers for the recovery systems depends on what stage of the vehicle, and thus what velocity it is returning from. From the video, it seems like the first stage is flying a "blastback" trajectory, meaning it returns to the launch site. Since first stages are not traveling very fast, it does not take that much fuel to do that, and you don't need much in the way of heat shielding. For example the Space Shuttle solid boosters really didn't have heat shielding. Air drag will slow you down some, so fuel used to land is not that much. I can't give any numbers without knowing the stage velocities.
The second stage and payload capsule are going much faster, and so need a substantial heat shield to come back from orbit or near orbit. You pay for carrying that heat shield with more fuel going up, but you still come out ahead if you do it right. The correct question to ask is "how much extra cost is the recovery system for each stage vs how much expensive hardware do I get back and can use again?" When working that question, you should factor in 2-5% loss rate from failures, rather than assuming 100% recovery every time.
I'm not sure I'll ever be able to see them as "retro" and less futuristic-looking than the shuttle, no matter how much more advanced and practical they actually are.
Doesn't matter. There's a good reason we don't use fancy Italian sports cars to haul our garbage. Function trumps style.
SpaceX has yet to put a person into space, let alone to the ISS, let alone returning safely, let alone a person on the moon.
All of this talk about how "SUPER CHEAP AND AWESOME IT CAN BE WHILE BEING PRIVATIZED" means NOTHING until they show that they can do it safely and repeatedly with a human being.
Take a look at the big island of Hawaii. On the west side you have a nearly constant slope formed by lava flows. You can build a "space gun" there with a barrel d = 20 km long. Assume you want to limit it to a = 3 g's (30 m/s^2) so humans can ride. The muzzle velocity is then sqrt ( 2 * a * d ) = 1100 m/s (Mach 3.6). This is in the range of what rocket first stage boosters do. The rest of the trip uses normal rocket stages.
Now assume what you are launching masses 100 tons (100,000 kg) and has a diameter of 5 meters. The pressure in the barrel then needs to be 153 kPa (22 psi). Gun is not really the right metaphor at those pressures, it's more like overgrown pneumatic tube. With the first stage taken care of, it is reasonable to expect 5% net payload, so you get 5 tons to orbit, which is enough to carry several crew.
Elon Musk has a new startup that sells an experimental weightless fuel.
I don't know about you, but I live fairly near the cape- and the last thing I want is half a rocket returning to Florida with... well, anything... not working.
It's rather easy to miss your mark when re-entering. It's even easier to miss your mark when you can't maneuver freely after heating. Things get worse yet still if the booster has a guidance failure or gimpy motor.
Don't get me wrong, I like the idea of a reusable rocket and I'm excited they are willing to try something so very, very ambitious. But I am certainly beginning to feel a bit of the "Not in my back yard" syndrome.
come clean, this is really k'breel, speaker for the council, isn't it?
the preceding comment is my own and in no way reflects the opinion of the Joint Chiefs of Staff
LOL
Yeah, right, let me know when this system is working as depicted.
For all the pie-in-the-sky science fiction shown in that CGI they should have at least made all three parts stack themselves on the launch platform ready to be refuelled and relaunched immediately.
Not in our lifetimes.
First stage usually do Mach 11. Orbital velocity is around Mach 25. Studied millions of times, never found economical.
Rail gun instead of cannon
Start way out at sea
100x reduction is cost to orbit?!? $500k tickets to MARS?!? Plus a (admittedly short) trackrecord of low-cost, successful engineering and reasonably successful launch history thrown in. And no obvious "throw money at us to play around with tech demonstrations" angle.
I want to know they're going to do it as much as the next geek, but they're out there trying to make it work. And have the business sense to not be 100% loony in those cost estimates, even if they're off by an order of magnitude. It basically costs me nothing to give them a resounding
"Hell, yes! Show me what you can do, SpaceX!"
(and please tell me more about how you plan to do it)
I was there for the talk, and had a little chat with Mr. Musk beforehand. The first thing to note is that he said that the video (which should go on their web page soon) is incomplete and may be vague about certain things, for proprietary reasons. What follows is my reverse engineering.
This is what the Grasshopper described previously in Slashdot is all about. Mr. Musk didn't use the word Grasshopper at all, so it must have been some sort of code word, but the tests in Texas will clearly be for Falcon reuse engineering.
Now, it makes no sense to return the first stage to the landing pad (as he said). The first stage is on a ballistic trajectory which (for a launch from Cape Canaveral) would have it impact somewhere far out at sea. It makes no sense at all to have the first stage reverse course and fly back to the Cape, as that would take as much delta-V as the original launch. It would make a lot more sense to land that stage in Ascension Island, Africa or Nova Scotia (depending on the inclination of the orbit). The first stage could then brought back by ship or plane.
The second stage actually goes into orbit, and the plan is to deorbit it one rev later. The trouble with that is the Earth rotates and the Earth will have rotated by ~ 20 degrees of longitude. That (again for a launch from the Cape) puts it over Texas, and it could conveniently land at McGregor, Texas, where SpaceX is doing their Grasshopper tests. So, although they haven't said so, I bet that McGregor will be the second stage landing area, and probably the Dragon landing area as well.
Look, the first stage doesn't just go up, it goes (presumably) eastwards to take advantage of the earth's rotation. So, if they launch from Florida the nearest land is, Africa. That means a foreign country and transport back by sea, not good for cost savings. If they launch from say California then you have all the hazards of a launch over land (isn't Vandenberg used primarily for westward ICBM testing and polar launches for this reason?).
Also, the second stage, even though it looks like it might go all the way to orbit doesn't appear to have much cross-range capability (no aerodynamic surfaces). So its choice of landing sites might be severely restricted. Finally, just to nitpick, the system isn't "completely" reusable, the service module looks like it is abandoned in orbit.
By the way, I think Elon Musk should henceforth be given the mantle of "Rocketman"! NOTHING (other than the heat shields) is used to slow down the stages AND CAPSULE other than ROCKETS; not parachutes or lifting bodies or airbags! He's got a LOT of faith that they will function in absolutely split second critical situations. WOW.
Still I say, go for it! If he can make the rockets work, maybe they can launch from that spaceport in New Mexico. (Maybe he'll have to give the FAA a destruct switch on a MANNED spacecraft in order to launch over populated areas). Has engineering gone so far as to really make these things that reliable?
i'm having final fantasy VIII flashbacks now. the Ragnarok launched via an electric driven rail and a ginormous ramp prior to it's rockets igniting. Normal spacecraft launched via a giant canon.
Your idea needs a new island... I don't think there are any Hawaiians too keen on putting much of anything on the big island.
"...And who wants to make buttprints in the sands of time?" ~Bob Moawad
Yes, this demonstrates the vast value of government. Throw a few hundred billion in, get a billion dollar rocket out.
I hope you were joking because the ROI on research dollars invested in NASA to the US economy is somewhere between 3X and 14X depending on which study you look at. There are over 1650 spin off technologies. NASA may run an inefficient manned space program but they are a genuine research powerhouse that MORE than pays for itself once you consider it's net effect on the economy. Just because the benefit isn't a direct one doesn't mean it isn't a benefit.
NASA can't do any of those things either. Even though it spends fifty to a hundred times as much as SpaceX for the privilege of not doing those things.
Science is all about firing a drunk pig out of a cannon just to see what happens.
When our name is on the back of your car, we're behind you all the way!
When our name is on the back of your car, we're behind you all the way!
A rocket lower stage isn't *that* big or heavy. Say it costs $500,000 to ship it back. That's still a massive win, right?
Any sufficiently advanced technology is indistinguishable from a rigged demo
--Andy Finkel (J. Klass?)
There's a better site in Ecuador. Also, gas guns are expensive and finicky.
A track made of conventional, passive coils carrying a sled cradle with either permanent magnets or conventional electromagnets gives a maglev which will be much cheaper. Use this to launch a reusable ramjet 1st stage which needs only about mach 1 or so to get going and you have either a shorter track or lower g-forces. The ramjet has much better Isp than a rocket and can be more robust and simple for reusability than a conventional rocket. This gets you up to about mach 5 at over 100,000 feet with a good angle. Either stage to a conventional rocket for a normal launch or switch to internal oxidizer to get to mach 13 and and rendezvous with a rotovator tether tip, transfer the payload capsule and land the 1st stage as an airplane. Fly the 1st stage most of the way back as a ramjet. Use a wing parachute for controlled low-speed landing, powered by the remaining fuel and oxidizer used in a smaller rocket engine. Landing gear can be light - no need to be able to raise gear, support high loads or high speeds.
"Is life so dear, or peace so sweet, as to be purchased at the price of chains and slavery?" - Patrick Henry
Why not use jets instead of rockets? If you're planning to land on Earth then there's plenty of oxygen at sea level, where you'll be landing. No need to lug all that cryo-oxygen around, just some avgas.