Intelsat Signs Launch Contract With SpaceX
New submitter jamstar7 writes "Following the success of the Falcon9/Dragon resupply test to the ISS comes the following announcement: 'Intelsat, the world's leading provider of satellite services, and Space Exploration Technologies (SpaceX), the world's fastest growing space launch company, announced the first commercial contract for the Falcon Heavy rocket. "SpaceX is very proud to have the confidence of Intelsat, a leader in the satellite communication services industry," said Elon Musk, SpaceX CEO and Chief Designer. "The Falcon Heavy has more than twice the power of the next largest rocket in the world. With this new vehicle, SpaceX launch systems now cover the entire spectrum of the launch needs for commercial, civil and national security customers."' As of yet, the Falcon Heavy hasn't flown, but all the parts have been tested. Essentially an upgunned Falcon 9 with additional boosters, the Heavy has lift capability second only to the Saturn 5. On top of the four Falcon Heavy launches planned for the U.S. Air Force this year, the Intelsat contract represents the true dawn of the commercial space age."
I am quite happy with the commercialization of space flight. I've always thought that the national space agencies were on the wrong path for decades. They always seem to aim for increased security and safety. I think spaceflight has gone over the top: the costs of increased safety are just not worth it. Commercial enterprises are excellent at making a proper risk assessment: certain risks are simply acceptable. This attitude is likely to reduce costs, which is what we need.
Obviously, NASA or ESA can still ask SpaceX to launch a couple of thousand tons of material into orbit, to assemble a Mars rocket and lander in orbit. :-)
When launching from Earth becomes easy, the next step can be considered.
Why does this story have the NASA logo
Maybe the Govt will sell NASA to Spacex
filthy one percenters!
Launching a two stage rocket to orbit is not exciting. Being able to build a tin can with a propulsion module is not exciting. I congratulate SpaceX for having done it, but it's not a major step forward in space technology.
Heavy lift vehicles are a big deal though. They change the nature of the game when you have them available. They really are exciting. Finding a way to commercially support their existence is the real exciting bit.
In a sense, it is something like the idea behind OTRAG - build big rockets out of smaller ones, so that you can commercially support huge lift capacity based on a market for smaller more regular launches.
The statement "The Falcon Heavy has more than twice the power of the next largest rocket in the world" is true but somewhat misleading. Both the USA and Russia have had rockets in the past with more than twice the power that the "Falcon Heavy" will.
Also, since this is in development, maybe the comparison should include other systems in development. Russia has a rocket with similar capabilities as the Falcon Heavy scheduled for launch at the same time, and China has a system under development" which has a lower low-earth orbit capability but similar lifting capability to geostationary orbit that is scheduled to launch a year later.
Four Falcon Heavy launches for the Air Force? This year? It's not on the launch manifest and quite frankly, I do not see the FH taking off for her first test flight before either very late 2012 or early 2013, so how can the Air Force launch 4 of them?
I don't remember reading anything about Elon Musk having trained as a rocket engineer, although his Wikipedia page mentions a degree in physics. Maybe that's enough to start a career blasting things up into orbit, much as Robert Goddard, Werner von Braun and the other rocket pioneers had no choice but to be self-taught. That or Musk's expertise is in designing rockets that look "cool".
I think the chinese one will be completed once the others have been completed and they have had time to "Evulate" their designs lol
and to get to geostationary orbit you need a load more fuel...
We've never added fuel to a rocket before! This is really going to increase the risk!
There's always some risk with doing new things. But SpaceX has demonstrated that they can do new things successfully.
This might sound strange, but guys like Intelsat avoid building satellites that can only be launched by one kind of rocket if in any way possible. Most geostationary satellites today cluster around 6 tons. This is the limit for the Russian Proton rocket (launched from Baikonur), the Ukranian/Russian/American SeaLaunch (using a Zenit rocket) and was the limit of the Ariane5 GS (which has been upgraded to the Ariane 5 ECA with about 10t. But ESA has a hard time finding customers for passenger satellites in the 2-3t range to make launches worthwhile.)
What does that have to do with SpaceX and the Falcon Heavy? Well, ESA is about to decide whether to develop a new smaller rocket - the Ariane 6 ( capable of lifting 3-8t to GTO) - or improve the Ariane 5 to the point that it can deliver about 12t to GTO. (With the idea of launching two of the popular 6t satellites at a time, which would instandly make the rocket much more economical)
In the latter case, SpaceX will have a much easier time to find heavy satellites for its rocket. Having a competitor is actually important in this business. You don't commit on the order of a billion dollars in building a satellite, just to find out that your only way to launch it is no longer available or recently had an accident (e.g. SeaLaunch or failures of the maiden flights of Ariane 5 GS and Ariane 5 ECA that also failed) and you have to wait several years to get another launch opportunity.
If ESA goes for the Ariane 6, SpaceX will most likely have to resort to launching several satellites at a time and compete with all the other guys that are also capable of launching "smaller" satellites. Which is bad for SpaceX and the industry in general. At the same time, ESA will find out that the old Ariane 5 will suddenly be in much larger demand for 8-10t satellites (as will be Falcon Heavy).
Lets hope they are reasonable ... or somebody comes up with something roughly similar to the Falcon Heavy.
they have had time to "Evulate" their designs
Did you mean: Evulgate
Ah, "they" referring to US and Russia, makes sense now. At first I thought you meant to say when the Chinese have had time to evaluate the others' designs, but instead I have learned a new word today.
The means that SpaceX will use to lower their price is to have enough launches that their fixed overhead becomes a minor issue. Right now, launches have a high fixed costs due to too few launches. SpaceX's plan is that FH launches once every 2 months and that F9 launches monthly or even twice a month. That allows them to drop not just the launch pad, but also their launch crew (who are typically on a salary, not hourly), as well as manufacturing costs.
To take this a step further, SpaceX intends to have 8 launches next year, and 12-14 in 2014. That allows them to have their QA under control as well. With this high of a rate, SpaceX will likely not need a back-up for the FH WRT launching sats. OTOH, if we are to go to the moon, we really need two or more systems of similar sizes. Or simply constrain the loads to the smaller of the LVs.
I prefer the "u" in honour as it seems to be missing these days.
The death rate of climbing Mt Everest is 1.3%. And that is just climbing a mountain. How much cooler is going into space? 10X?
Now at this point in my life where my family is depending on me 1.3% is too high. But when kids are older and I can be more selfish 5% doesn't sound that bad. Like everything else it's a personal decision.
http://wiki.answers.com/Q/What_is_the_death_rate_on_mt._Everest
I love Jesus, except for his foreign policy.
A Saturn V sitting on the lawn of Johnson Space Center doesn't count, neither do Shuttle orbiters on display at various museums.
25k and 40k kg to LEO are a bit far short of the 53k kg of Falcon 9 heavy. Also I hope they get a bunch of launch contracts for Falcon 9 so they can fund the $1B they need for Merlin 2, it will be the first engine to produce more thrust than the F1 from the Saturn 5.
There are 4 boxes to use in the defense of liberty: soap, ballot, jury, ammo. Use in that order. Starting now.
"On top of the four Falcon Heavy launches planned for the U.S. Air Force this year (...)"
Uhm, what? Falcon Heavy's first flight is scheduled for 2013 and it will be a test flight, I doubt it will carry any commercial cargo. Maybe the planning for the US Air Forces launches was done this year, that can be true, but I'm certain that no Falcon Heavy will lift-off in 2012.
yes! if they were allowed to die. The business cycle has been overridden by gvmt lately...
pure capitalism is painful and ugly and has all sorts of undesirable side effects -- but it wins!
Am I mistaken or will the Falcon Heavy have 27(!) engines going at liftoff? (3 x the nine engines of a Falcon 9).
I guess they really have the control systems for such a large number of engines licked (in a previous thread I noted that back in the 60s the Russian Moon super-rocket N-1 had 30 engines. It failed, repeatedly.)
So are large numbers of small rockets preferable, efficiency wise, to a few large ones (think the five F-1s of the Saturn V first stage). Or they cheaper in aggregate? Or are they more reliable? (less superhigh pressures in the turbines, I dunno). Or if they fail is there the simple fact of more redundancy (I read that if any one of the Falcon 9s engines conked out it could still make it to orbit. Except right at lift off).
Or did Space-X just not have the funds to develop a really big engine (In which case couldn't they have licensed the design for the F-1 or J-1 from NASA?). Not knocking them, it's still an INCREDIBLE achievement, just wondering.
To quote an Airforce General: "A new plane doesn't make possible a new engine, a new engine makes possible a new plane.". So it's great to see an (obviously) flight worthy new rocket engine!
so you don't have to use the NASA icon for every SpaceX story.... of which there's gonna be many in the future
By that logic, the falcon heavy doesn't count either, it doesn't even exist yet. Unless you are claiming that pictures on a screen have more thrust than an actual physical rocket?
... the Intelsat contract represents the true dawn of the commercial space age.
That's right, folks, it's Morning in America!
"Somebody has to do something. It's just incredibly pathetic it has to be us."
--- Jerry Garcia
Space-X has a new engine in the design phase that will have 1.7 millon lbs of thrust. The Merlin-2 engine will be more powerfull than the Saturn-V's F1 engine was. The Falcon-X heavy will use 3 of these engines per core, or 1.5 times the lift of the Saturn-V. The Falcon-XX heavy would use 6 of these engines per core, for a total of 18 engines. It would have over THREE times the lift of the Saturn-V rocket! http://en.wikipedia.org/wiki/Falcon_%28rocket_family%29#Merlin_2_and_super-heavy_lift_concepts
Unless you are claiming that pictures on a screen have more thrust than an actual physical rocket?
LOL. Powerpoint rockets always have more thrust.
Hey, it worked! Okay, so what's the price difference in their rockets vs traditional US airline companies? What? Everyone is hopping on board now that it didn't blow up or crash into the space station and I do hate air travel, lol.
From TFS: On top of the four Falcon Heavy launches planned for the U.S. Air Force this year, the Intelsat contract represents the true dawn of the commercial space age.
Only if you somehow handwave away the decades we've already had of private companies contracting with other private companies for launch services.
And she'll make .5 past light speed....
all that information is from a presentation by a (now) former SpaceX employee which was disavowed by the company as 'paper plans'. there's no evidence either way that any of that stuff is in progress.
The various press releases are forgetting something. The Falcon Heavy is third in lift capability behind the Saturn V and the Energia . Granted, the Energia only had two flights before the collapse of the Soviet Union made it too expensive to operate, and on one of the the payload malfunctioned after separation and deorbited itself almost immediately, but in both cases, the booster functioned just fine. It was capable of lifting 100 metric tons to LEO (which was more than enough to give the Buran, the Soviet space shuttle, a piggy back ride to orbit), which puts it just shy of Saturn V's 118 tons, and is almost double the Falcon Heavy's 53 tons.
#include <signature.h>
Elon Musk, SpaceX CEO and Chief Designer
Congrats to SpaceX, but can we drop the bullshit?
If Elon Musk designed anything more potent than the paint scheme on the side of the rocket, then I'm the Pope.
I just looked again at SpaceX's announcement and saw that they claim the Heavy will put 53 tons in LEO or "more than 12 tons" into GTO.
Well unless the "more than 12 tons" is a lot more than 12 tons, it means you're only getting 1/4 the payload into GTO that the same launch vehicle can put into LEO. That's terrible! (to me). Wasn't it Heinlein who said get to earth orbit and you're halfway to anywhere? Seems like you're only a quarter of the way. Also, GTO (Geo-sync Transfer Orbit?) isn't even all the way there yet, you've still got to circularize the orbit otherwise you're just in a big ellipse. So your profit margin I mean payload is even smaller.
I don't know if this is due to some peculiarity with the Heavy or its launch site (Geosync orbit is on the equatorial plane) so maybe with other launch vehicles/launch sites it isn't so bad (now I know why the ESA uses their jungle launch site). Still, I'm thinking that those systems still can't do that much better.
There REALLY is a crying need for an efficient, powerful (high) thrust ion engine system that will cut this ratio down to less than 2:1. 26 tons to Geo sync (or escape) and you're talking big useful payloads. For science think Mars sample return or Europa sub. For commerce think worldwide wristwatch satellite phones (big antennas in space = little ones on earth). It needs to be (relatively, for an ion engine) high thrust so it'll take months and not years to get there. Of course you'll need some big-ass solar arrays but remember, once you get to your destination (or coasting when your engine is off), you can use all that electricity for your spacecraft and powerful transmitters.
Really? What about the center core propellent cross-feed? That sounds like a major piece that cannot have been launch tested yet. AFAIK there is no other rocket that has ever had it either so there must be some element of risk. All that mass transfer could go wrong in any number of ways I suppose.
Mentioned in the blurb:
One should note that you could put up 10 Falcon Heavy launches for less than the cost of 1 Saturn 5 in 2012 dollars, roughly calculated to be on the order of $ 1.17 billion per launch of a Saturn 5. That's a couple hundred million under what NASA is paying for 12 Falcon 9 launches.
Understanding the scope of the problem is the first step on the path to true panic.
[url]http://www.fullripindir.com/[/url]
"All the science I don't understand, its just my job five days a week" -Elton John
first? No.
By that logic, the falcon heavy doesn't count either, it doesn't even exist yet. Unless you are claiming that pictures on a screen have more thrust than an actual physical rocket?
The difference is that the USA manufacturing industry is up to the task of building a Falcon 9 Heavy launcher, while building a new Saturn V exemplar is right out. (Tooling lost, skills lost, experience lost, blueprints (possibly?) incomplete etc.)
Ezekiel 23:20
See http://cosmiclog.msnbc.msn.com/_news/2011/07/13/7078446-spacex-chief-aims-for-mars?lite
Look at the price range that Spacex quotes for a Heavy - from $85 million all the way to $125 million. That tells me there is more than one version of the Heavy. I believe the GTO specification on the website was done specifically for Intelsat and refers to a downrated Heavy (a Medium?) with probably about 4 engines on each strap-on, with proportionately shorter tanks. The strap-ons are quite simple (no nav system, no steering capability) so the major cost for them is the engines. Hence reducing the number of engines would reduce the cost.
Note that I am assuming the strap-on tanks can be shorter. They can't change in diameter because they have to fit the launch facility. However I think they can be shorter because the Heavy has propellant cross-feed, so they can fill (or drain) the strap-ons via the umbilical connection to the core. I am assuming they also cross-feed nitrogen for purging, electric power, and whatever else they need. But even if they can't be shorter they can just be left partly filled to reduce lift-off mass.
- Gord Deinstadt