SpaceShipTwo Design and Pics Released
An anonymous reader writes "Designs and photos for Scaled Composites and Virgin Galactic's new suborbital spacecraft, SpaceShipTwo, and its carrier aircraft, WhiteKnightTwo, have been released." Lots of specs and numbers if you're interested in that sort of thing although nothing hugely detailed.
Really, the primary thing this project has going for it is that it is not funded by a government. It might be boring and not state of the art now, but further development of private space flight should lead to some truly interesting technology and vehicles.
Cutting edge technology is only one place to contribute to space flight. Production improvements can also aid space flight, and producing more of the material needed to do space flight may improve manufacturing techniques.
Then making 'space flight' available to more of the public helps create more awareness.
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I should add that I'm only criticizing SS1/SS2. I have nothing against WK1 or WK2; they're quite nice carrier aircraft. But SS1 and SS2 are completely meaningless. If you want small companies doing meaningful rocketry, check out SpaceX. Their Falcon 9, a rocket whose heavy version will carry as much payload as NASA's beleagured (and possibly dead in the water) Ares, including its own spacecraft that can dock with the ISS, will be launching this June. The typical launch cost of payloads in the west is $10k/kg. In Russia, China, and India, $7k/kg is the standard. Sometimes you can get discounts down toi as low as $4-5k/kg. The Falcon 9 is $2-3k/kg. And looking over its construction, design, stats, etc, these numbers definitely appear credible.
Cheer for the rocketry not matters, not the irrelevant joyrides.
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For a bit of perspective I wanted to see what progress looked like back in the early days of aviation.
http://www.aerospaceweb.org/question/history/top10/wright-flyer.jpg Here is the wrights' "space ship one"
http://www.dkimages.com/discover/previews/786/506847.JPG Here is what the aircraft started looking like 4 years after the Wright's first flight.
It took 30 years for Jet technology to appear, I wonder if it will be a similar amount of time before we get private orbital cabability.
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More pix: http://www.virgingalactic.com/pressftp/
Maybe we should all chip in and buy them one of these: http://www.angryflower.com/aposter.html
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But, really, if private space travel is to become commonplace, what we want is boring and un-sexy technology -- not exciting and cutting edge.
What we need is the equivalent of a Buick station wagon with wood-grain trim. Boring as hell, but a reliable vehicle which focuses on doing the task instead of pushing the envelope. Once you have that, then this stuff can start to become routine based on available technology.
Cheers
Lost at C:>. Found at C.
Say the 29' Mercedes was far more impressive technically than what Ford was putting out but how many straight 8 engines do you see used in cars today? The most cutting edge isn't always the most practical. Do we wait for warp technology for space flight or use chemical rockets to get the ball rolling? The Space Ship 2 is the Model T of space flight. That's not an insult it's a major compliment. The Model T was one of the most successful cars in history for good reason. This craft puts space flight not into the hands of the average person but potentially into the hands of large numbers of people. Henry Ford would give it a big thumbs up and we should all view it as the stepping stone it is.
I'm surprised at the amount of scepticism over this project, esp on /. Let's face it, commercial designs such as SS2 are the only way any of us down here will be getting 'up there' in our lifetime.
FYI, from el Wiki: "More than 65,000 would-be space tourists have applied for the first batch of 100 tickets to be available. The price will initially be US$200,000. However, after the first 100 tickets are sold the price would be dropped to around $100,000. Then deposits after the first year will drop to around $20,000. The duration of the flight will be approximately 2.5 hours, and weekly launches are planned.
In December 2007 Virgin Galactic had 200 paid-up applicants on its books for the early flights, and 95% were passing the necessary 6-8 g centrifuge tests"
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- Mike
Once you've lost your temper, you've lost the argument - Me
Probably half or more of the posters here are from America. If you check a number of polls, many Americans believe that NASA has been a waste. Sadly, they also believe that Science is a waste. It comes down to the more that politicians declare that science projects like Genetic Engineering, Stem Cell research, Global Warming Research, etc is bad for the world (and America), then by extension, then RD efforts like NIH, CDC, and even NASA must be worthless. Out politicians are killing us. It is no wonder that we see our RD labs torn down.
I prefer the "u" in honour as it seems to be missing these days.
This is not about advancing the state of the art in rocket design, no one ever claimed that it was.
They are learning how to build an infrastructure that could take paying customers to orbit.
They are gaining experience carrying passengers and a spaceship up to the edge of space.
They are gaining experience dealing with novice 'astronauts' and what it takes to prepare them and what they should expect from them in a weightless environment.
They are gaining experience designing and building and flying carrier aircraft.
I would imagine that the next generation will use a different rocket design, go significantly faster, and start using heat shielding, with yet a bigger carrier aircraft.
Once they have that in place, the next generation can upgrade the 'spaceship' to something with serious rockets that have the capability of reaching orbital speeds.
Or should they have gone for orbit first and hope everything else works at the same time?
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Imagine a ski, versus a wheel.
It's simpler and more lightweight. Less moving parts. Also probably a lot easier to package.
Virgin is focusing on a specific limited mission that no one has done in a way as to open it for a large number of people. If Virgin can make money giving people these cannonball shots, then others, if not Virgin itself, will spend the money to research and develop a craft that can do orbital or even lunar missions. There doesn't need to be a linear progression from SS2 to an orbit capable craft. My analogy was fine because I don't think the Buick should be on the racetrack. They are vehicles designed for different tasks; tuned to their specific environments; just as orbital and sub-orbital missions are different. Again, all Virgin needs to do is to make money doing this. Then people will believe that a NGO can do this, and NGO orbital fights will come with a craft properly tuned and designed for that more difficult challenge. When that happens, you will see the new technology.
As to my understanding of rocket science, well, for starters, maybe you should learn manners before you return to the discussion. You're not going to convince people to agree with your opinion if you insult them first. You only come across as an idiot when you do it; regardless of how smart you may be. You also might try opening your mind to ideas that don't fit with your own narrow view of the world.
- Mike
Once you've lost your temper, you've lost the argument - Me
***This was a very good point, IMO***
**quote**
As I mentioned before, I was in error about how much delta v it takes, including gravity losses, to get in orbit, 9500 m/s instead of 11km/s. So about a quarter of the necessary delta v was provided by the motor and a further 300 or so m/s by the plane. Given that SpaceShipTwo goes a bit higher and has more downrange than SpaceShipOne, it probably has a little more delta v. So you're too low by at least a factor of 2 in your delta v estimate. And there's still higher ISP fuels. For example, they can use liquid oxygen in their hybrid to boost ISP. And higher mass ratios will obviously be needed. But I see no reason orbital delta v can't be reached.
****
Twice the thrust is probably attainable with more engines(check) and a little more fuel that has a higher energy output(I hate acronyms - a pet peeve of mine). The ship itself that launches them can also without a doubt be made to go faster, especially not IF, but WHEN we get scramjets and similar technologies working. 4000m/sec from the module and 1-2000m/sec from the booster/plane/etc is suddenly not so far off the mark.
IME, when you start talking about engineering problems and the difference between making it happen and the prototypes is a matter of 2-3x the test results, it's a matter of figuring it out more than being in the realm of "not possible". I don't think Scaled Composites second design can get into orbit, but it's a good step in the right direction, make no mistake about it.
I have to give them props for trying at least. Their goal is to get into space and not just give joy-rides, after all.
> If you disagree with this statement, go ahead -- explain why you feel that a vehicle with this low delta-V, horrible ISP, and proportionally high mass that faces bare minimal reentry heating -- advances the state of the art.
Other than contributions like feathered reentry I agree that it does very little to advance the state of the art.
But that is precisely the point. The state of the art does not need much advancing. Everything we really need know in order to get into space has been known for a couple of decades and has advanced very little even with much bigger budgets thrown at it by governments around the world. What we need to advance is the state of practice and Scaled/Virgin is doing exactly that.
Just one small example: an aircraft capable of carrying with proper ground clearance and safely dropping this size of load did not exist until now. It can be useful for many other applications like this one. Does this advance the state of the art? Of course not. We've known such an aircraft can be built for well over half a century. But having this kind of aircraft actually available shaves many millions and a lot of risk from the budget of projects that need it. We all know these projects are facing lots of risks and are always underbudgeted so every little bit of help they can get really counts.
So it has been funded by joyriders. Anything wrong with that? Would you rather fund such development with your tax dollars?
Stop worrying about the risks of nuclear power and start worrying about the risks of not using nuclear power.
Twice the thrust is probably attainable with more engines(check)
1) It's not "twice"; it's level of performance is a tenth that of what is needed for orbit.
2) Thrust is not the problem; it's ISP and staging.
and a little more fuel
Try a hundred times more fuel and a craft equivalently large enough to manage it. See OTRAG for details.
that has a higher energy output(I hate acronyms - a pet peeve of mine).
Nobody who discusses rocketry any relevant amount will spell out the words "specific impulse" every time. It's just "ISP". Insisting on spelling everything out marks you as a novice as much as I'd come across as an internet novice by constantly spelling out www as "world-wide web".
The ship itself that launches them can also without a doubt be made to go faster, especially not IF, but WHEN we get scramjets and similar technologies working.
Lol. Just, lol.
4000m/sec from the module and 1-2000m/sec from the booster/plane/etc is suddenly not so far off the mark.
What is off the mark is that Scaled is going to go from polybut and nitrous to an as-of-yet in-development technology that requires carbon-carbon panels and an extensive regenerative cooling system with typically hydrogen fuel, without completely starting from scratch to boot.
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Right, SS1/2 aren't even close. That's not why they are interesting. You don't expect a Buick to win a Formula-1 race, or even be competitive.
;) Of course, the reality is likely that the materials science is not be there yet, and one just can't build a useful rocket using low-tech parts yet, but I glad to see someone at least trying.
Further, the team isn't even *trying* to advance the state of the art in any fundamental science.
But that's why it's interesting. This is a low-tech engineering approach, with as close to commodity parts as they can manage. They're still a long long way from anyhting useful, but if they ever do get there they will have knocked a couple of 0s off the price, and significantly reduced the engineering complexity.
Naturally that provokes hostility from real rocket scientists - hey, the next thing you know, rocket science will be simple enough to outsource to India.
And the Penske team did famously win an Indy-car race with a very low-tech Buick-like engine once (pushrods for the win!), but that's a different story.
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