Battle of the Heavy Lift Rockets
schwit1 writes: Check out this detailed and informative look at the unspoken competiton between NASA's SLS rocket and SpaceX's planned heavy lift rocket. It's being designed to be even more powerful than the Falcon Heavy. Key quote: "It is clear SpaceX envisions a rocket far more powerful than even the fully evolved Block 2 SLS – a NASA rocket that isn't set to be launched until the 2030s." The SpaceX rocket hinges on whether the company can successfully build its new Raptor engine. If they do, they will have their heavy lift rocket in the air and functioning far sooner than NASA, and for far less money.
There have been way too little competition in this area the last decades. Considering that the Russian RD-180 engines designed in the 70's&80's are still seen as state of the art it is obviously a stagnant situation.
If builders built buildings the way programmers wrote programs, then the first woodpecker would destroy civilization.
Mr. Mueller then later updated his numbers at a follow-on conference to portray 6,900 kN of sea-level thrust, and 8,200 kN of vacuum thrust.
That took me 20 seconds to find.
Come on, its Slashdot, at least give us some technical information to back up the story.
TAILS opens an official public mailing list with archives!
Personally, I prefer Sonic.
If anyone can get it done, it will be Elon Musk and SpaceX. They have the vision and agility that NASA lost in the sixties.
NASA never wanted to build this rocket. It was forces in them from Congress. Plus NASA doesn't build rockets it overseas other aerospace contractors.
I love Jesus, except for his foreign policy.
Pork barrel NASA rocket to launch pork barrel NASA missions vs SpaceX building a rocket that is of no use other then for pork barrel NASA missions.
Just because the latter has less pork doesn't mean it's good.
I mean seriously, look at the SLS, it's almost entirely composed of re-used space shuttle parts. It has the main engines on the bottom of the tank re-purposed from the shuttle. it has solid rocket boosters which already exist from the shuttle -- it entirely looks like it could be cobbled together in a few month's time because it uses almost entirely existing components.
So what exactly requires so many years to make it al work when it's all basically existing tech from the shuttle? I hate to say this, but this ain't rocket science.
If telephones are outlawed, then only outlaws will have telephones.
They burn something like 99% of their takeoff weight just to get to orbit. Their biggest cargo is their own fuel.
Where's the research on mass drivers/railguns, or tethers, or any of the "scifi" types of propulsion?
I want to delete my account but Slashdot doesn't allow it.
Methane-fueled rockets burn brilliant blue. It will be a sight to see.
NASA would be very happy to let SpaceX build a heavy lift booster for them. Really.
The only reason SLS exists is to keep the congresscritters from the former shuttle supply chain districts happy. That's it. NASA is desperately trying to keep funding going, and they ain't interested in pissing that money away on designing big dumb rockets, but politics says that they must to survive. Rockets are rapidly becoming a commercial technology, which is a good thing.
NASA would be very happy to buy rockets from Elon Musk and/or whoever else can put up competing articles. NASA would much rather be doing and spending its hard-fought budget on things that they do well, pushing the envelope on technologies for hard problems, like getting our asses to Mars, and science missions.
Left MS Windows for Linux Mint and never looked back!
Vote for Bernie in 2016!
It's been the better half of a century that we realized using chemical rockets to operate outside of Earths gravity well is a fools errand. I'm rooting for Musk, but he is 1 spectacular explosion away from irrelavancy. While we wait for the inevitable, I trust the Chinese will rediscover the idea of space stations and building stuff in orbit while we wait to discover a way to catch up with an entire universe that is fleeing from us as fast as theoretically possible.
Still, being only one (or two) generations removed from the most savage and disruptive warmongers the planet has ever seen is enough justification for any man of true freedom to use any meañs possible to get as far away from the king as possible. The truth is, I would rather die on Titan in 10 years than to have to endure the Marxist-Fascist coallition that the peasants of the world have deemed "good enough"
TL:DR - we're fucked.
There are no miracles in rocket engine design. The RD-180 has pretty much the best performance to be wrung out of a sea-level-to-altitude LOX/RP-1 motor in terms of efficiency. SpaceX is still playing catchup in that area, trading off the lower cost per Merlin motor for a lower Isp from a simpler design.
As for the Raptor the "new" liquid-methane/oxygen fuel mix it will burn has the potential to produce a higher Isp than the current mainstream LOX/RP-1 mix used in motors like the Merlin, the RD-180 etc. but it comes with downsides -- it means a redesign of the rocket structure to support fully cryogenic tankerage (although not requiring the sorts of extreme temps or processing LH needs), launchpad facilities for fuelling and defuelling rockets will need to be revamped, liquid methane is half the density of RP-1 so the tanks and the rocket structure need to be larger and heavier to contain equivalent amounts of fuel and so on.
http://www.cbsnews.com/news/ne...
We are on the verge of a global energy & debt crisis. The Era of space flight is coming to an end. CapEx in Energy development is coming to a rapid decline. No one can afford $150 bbl Oil and the Oil companies are ending development of future projects need to offset depletion. Within 12 years the world won't be able to launch satellites.
Not that long ago (perhaps last year) there was a news item about a new rocket design from Europe that, according to that new piece that I read, offer much powerful rockets while still save fuel
Do not have the link to that news item (maybe deleted) but if anyone still have the link, please post here
Thanks !
I Don't no https://www.youtube.com/watch?...
For those of you who visited the link, Nasaspaceflight.com has a very well-informed stable of posters, many of whom are professionals in the space industry, and there is the L2 section where you will find much that is not available anywhere else.
One thing people forget, is that the Private sector, can often do things a great deal faster as there is way less red tape. In the Public Sector, you have to have more justification on who you buy everything from, to contractors, everything. The public sector is greatly hindered by this in so many ways, to make sure everything is above board, and fully transparent, and it only gets worse as the economy gets worse, as the government wants an accounting for every last penny, because they believe the public really will care on which toilet paper is being used by government officials. Also if something is not on a standing offer for the government, it must go to be bid on by businesses.
There are two measures of rocket engine performance: Isp and thrust-to-weight. RD-180 has about 10% higher Isp than the Merlin 1D, but the Merlin 1D has DOUBLE the thrust-to-weight of the RD-180, which is why they're putting together a rocket with it that can launch over 50 tons to LEO (the Atlas V is dependent on costly solid rocket boosters for many payloads, and even the proposed heavy configuration using three cores would launch under 30 tons to LEO). Thrust determines how big you can make your propellant tank, which determines how big your payload can be. When SpaceX bumped up the thrust they could get out of their Merlin, from the 1C to the 1D version, they also gained the option of stretching the Falcon 9, considerably increasing its payload capacity. SpaceX isn't chasing RD-180 performance, ULA is gnawing their fingers with envy at the Merlin 1D, which can even be throttled precisely enough to land the rocket!
Raptor is going to be the first real 21st century rocket engine, with 3d-printed parts and fluid bearings (rather than the primitive old ball bearings used in other rocket turbopumps). They aren't going to methane for the Isp boost (which would just not be worth it, considering the lower density), but because liquid methane can be self-pressurizing (no high-pressure helium system) and costs about one tenth of what RP-1 does. In addition, it's stored at very nearly the same temperature as the liquid oxygen, which simplifies thermal management. The full-flow staged combustion design is also not primarily for Isp (though it will provide a high Isp), but because of the low temperature of the working fluid, which means you can use cheap materials in the turbopump and it will last practically forever.
The reusable Raptor-powered BFR will likely cost less to operate than the reusable Falcon 9, with a longer service life. Even the manufacturing cost may be lower.
There are a fair number of ex-NASA folks at SpaceX.
However, there's also a fair number who went, and then disappeared away from Space-X. The environment at SpaceX is pretty aggressive development schedule (work-life balance? As long as you're alive, you can work, stop your whining.). The NASA engineer who gets frustrated with the slow pace at NASA might find it fun at SpaceX. The engineer who likes working on lots of different things at NASA probably won't like it at Space-X.
Point the rockets at each other, nose-cone to nose-cone, ignite them both and let's settle this once and for all; Mortal Kombat-style!
(or at least, Celebrity Deathmatch style)
The Good: We could end-up with two extremely-capable heavy lifters that launch from separate facilities (excellent and complete redundancy) which could enable a bold new era of exploration. Just imagine the missions you could fly by having NASA park a mars transit vehicle in orbit and SpaceX dock a massive fuelled Earth departure stage to it, perhaps with the crew flying up to it aboard a DreamChaser launched on an Atlas (Maximizing the non-crew related weight the heavies could loft). Mars mission in three launches, possibly all on one day. These systems COULD all be used in concert with each other (more important givien that Obama's NASA is reducing to one pad (39B) and therefore will be incapable of using SLS alone for any significant deep space manned exploration (that would require multiple launches and it taked too long to refurb a pad to be able to do this with one pad).
The Bad: Morons might use this to convince congress to kill SLS (dreaming that the cash would be re-directed to SpaceX or elsewhere in NASA when the politicians whould actually be likely to shift it no non-space priorities). With a down-scaled and further funds-constrained NASA, SpaceX could then lose its main customer and never end-up actually being able to afford to build their giant. A similar scnario nearly happened when some people with an idea they called "Direct" advocated killing the Constellation program and funding their project instead - and the Obama admin DID kill Constellaion (and then proposed NOTHING to replace it, rather than the "Direct" project - which is partly how we got to the mess we are now in where congress is pushing SLS and Obama keeps trying to kill it).
The big problem with all this SpaceX fanboy stuff: SpaceX is cool but has demonstrated NO ability to keep to a launch schedule and has a history of claiming it will build and fly rockets that it never actually does build and fly. Remember Falcon1??? How many here remember Falcon5???? Does anybody here remember how many Falcon9s were supposed to have flown to ISS by now or how many tons they were contracted to deliver? (hint: more, and MANY more) Has everybody forgotten that Falcon9 Heavy was supposed to be operational by now but is still only on the drawing board? Do people forget that the current Falcon9 is VERY different from the Falcon9 that flew the first flights? Does even the new version meet the original promised performance specs for Falcon9? I like SpaceX and wish them well and LOVE the fact that they are putting flood lights on the lazy, bloated, over-priced and under-innovating traditional rocket builders BUT this does not change the fact that they have not provided any evidence yet that they will be able to build such a giant rocket, deliver it on ANY schedule, fly it on ANY schedule or have it perform anywhere near to the specs. IF SpaceX beats NASA into space with a super-heavy rocket it will likely NOT be because SpaceX has met its promises but rather because NASA and Boeing have wallowed in incompetence and slipped their schedules so badly that they end-up falling behind Musk (as opposed to Musk beating them by being excellent and speeding-up to overtake them). Sadly, THIS is the scenario that we have the evidence to support.
or some other boringly predictable rant.
spoiled children have been ranting about the grownups making them act right ever since the dawn of recorded time.
RD-180 flew it's first flight in 2000, and it's based on RD-170 which flew it's first flight in 1987.
So not designed in seventies.
AK-26 / NK-33 (used in Antares rocket) is the engine developed in sixties and manufactured in seventies.
RD-170 is more powerful than F-1. Though it's multi-chamber engine.
Space shuttle solid boosters are also much more powerful than both F-1 and RD-170.
F-1 is the most powerful single-chamber liquid-fuel engine.
Dou! The thing is if you want to put all this stuff into orbit -self running autonomous factories and so on - the first thing you will need is a bigger rocket - a much much bigger rocket. (like 100 or 500 tons to GEO or more) What we really need for the expansion into space whichever way we do it is a rebuild and reimagining of something like the old 'Sea Dragon' project. If you want to move a lot of cargo (or hundreds of passengers) you need to build big.. Its Simple!!!
Below the speed of light Special Relativity is one of the most accurate theories in physics - above the speed of light..
Even more motivation to defund SLS...