SpaceshipOne's Control Problem Fixed 230
Baldrson writes "Wired News reports that Rutan's team says they have gotten to the bottom of the June 21 flight anomalies that affected the first SpaceShipOne sub-orbital flight: 1) A control surface actuator had run against a stop limiting its movement, and 2) Wind shear caused the 90-degree roll shortly after rocket ignition. Rutan also said with the problems now identified, the next time SpaceShipOne flies, it will be to win the prize."
JC (Score:2)
Re:JC (Score:5, Informative)
According to John there is no other team even close, and I believe him.
Impressive (Score:4, Insightful)
Between the private space-flight, a entire space station (built internationally no less), and the possibility of a space elevator, humankind really is heading for the stars!
Re:Impressive (Score:5, Interesting)
Actually, that's one of the things I really admire about Armadillo Aerospace - they've kept very little to themselves - anybody with some money, patience and skill could get going quite quickly by learning from the Armadillo website.
Re:Impressive (Score:4, Informative)
Nobody considers Armadillo anywhere near close. The other team that's close is Da Vinci project. They are the only other team that's actually got hardware constructed with any amount of testing (photos) [davinciproject.com] done on it. Thier schedule calls for the first sub-orbital test flights in august of this year, and they are the only X-Prize team other than scaled actually planning to fly this summer. they are also the only other team that has minor details like launch permits etc all wrapped up.
Re:Impressive (Score:4, Insightful)
Unfortunately, as far as I can tell, Armadillo isn't even using a fuel - it looks to be a straight peroxide rocket, as I haven't seen them mention a fuel since May 2003. So, not only do you have a chemical that's hard to work with, you have a very low ISP, too. I'd never dream of going that route. Not that I think that Rutan's choice of fuel and oxidizer are all that incredible (why on earth NO3 as an oxidizer???), but they're better.
Also, vaned thrust deflection instead of gimballing, while it may look great on paper, just seems like a problem waiting to happen, as far as rockets go. It's no shock that they've been having big problem with that system... it's fine for jet engines, but with rocket engines, you're dealing with far more intense, far hotter exhaust in a high vibration environment. Also, vaned thrust deflection loses more energy than gimballing due to drag, which is something that they just can't afford, especially with a monopropellant rocket.
In short, I don't much care for their design.
Re:Impressive (Score:4, Informative)
Armadillo was using high purity non-stabilized peroxide up until roughly a year ago. It does not need injected liquid catalysts: just using silver and platinum, or various other solid catalysts, works just fine.
Now, Armadillo is using a mixture of 50% unstabilized peroxide and methanol. It has about the same energy per unit mass/volume as 90% peroxide does, but is a fraction of the cost and handling issues of 90% plus unstabilized peroxide. Still a monopropellant, but very much simpler and cheaper.
Please read harder. Armadillo has been describing their rocket motors in detail repeatedly.
Isp is not everything. For a first stage, density impulse is much more important. And for a non orbital rocket vehicle, handling and ease of design and construction are also very important.
Amateurs talk Isp; Professionals start with density impulse and then system design tradeoffs on the overall vehicle; Experts talk development cost and timeline to get vehicles that meet the minimum requirements flying successfully.
Not NO3. N2O; Nitrous Oxide.
Why? It's not a bad oxidizer, that's why. It has less oxygen than LOX or peroxide or nitrogen tetroxide or nitric acid, true. But like peroxide and hydrazine, it's got internal energy, so when it starts to react the dissassociation adds energy to the reactions. That evens it out. Nitrous is decent overall performance and self pressurizing, which none of the other oxidizers are.
Again: Specific Impulse is not everything. It's a lot simpler, safer, easier to develop a vanes system than a fully gimballing motor. Less mass is moving, no propellant lines are moving.
Real rocket innovators have been looking at jet vanes on and off continuously for the last decade. Most chose to go another direction, but they are not a bad choice for certain sets of vehicle design and development assumptions. Carmack's group called that one right: it is a good choice for their vehicle and their development program.
Well, fine, but at the very least you could read up on the actual details and see what other people who actually know something about rocket design think about it.
I would never have developed exactly their vehicle, however, Armadillo are making incremental good choices and have a clue about both ultimate performance and doing development on
Re:JC (Score:2)
Re:JC (Score:5, Informative)
Serious X-Prize contenders realized early on, there's a lot of rocket technology available 'for sale' out there. They bought rocket engines, and concentrated on the difficult part of the engineering problems, the vehicle to get into space and back.
There's 2 teams that have a chance of actually completeing the X-Prize flights this year. It's interesting, Scaled has used the 'all aerodymanic' approach, with a mothership for first stage lifting to get above troposphere. Da Vinci project is 'all ballistic' with a mothership to provide first stage lift above troposphere.
Scaled is currently the odds on favorite to achive the X-Prize flights first. They have a really good chance, they have all the flight hardware, and it's been thru rigorous testing. Still, manned space flight is HARD (just check with Nasa for reference), and it's NOT a given that the SS1 + WK combination can complete 2 more flights without incident. A serious incident with either vehicle, and Scaled will be out of the running for the X-Prize, there isn't time left to replace either of them.
Da Vinci project has flight tested engines, but, they have yet to flight test an all up final configuration. They have the permits in place, and, the hardware is built. They are expected to start flight testing within the next 6 weeks.
Armadillo, well, they are tinkering with rockets, and writing a blog about it. They dont have a vehicle to mount an all up configuation rocket in, and they dont have a design to build one from. The X-Prize must be claimed this year, and Armadillo hasn't even got a vehicle design yet. No, they are not in the running, and have no hope of being in the running. If you haven't done the engineering analysis on a design, to validate it should be capable of withstanding the launch/recovery portions of the flight, and got the hardware built, ready to fly this summer, you are not in the running for the X-Prize. No matter how much money you throw at it, you are not going to design/build that package in the next 4 months, and if it's not flight ready in 4 months, you cant meet the requirements for winning the X-Prize.
Re:JC (Score:2)
I don't know what their problem is. (Score:5, Funny)
Re:I don't know what their problem is. (Score:5, Funny)
Sure, take the easy way out winning the xprize by launching 100km up from the moon
free trust_based image hosteing [sharkfire.net]
I don't get it ... (Score:4, Interesting)
"the actuator delayed moving one of the ship's flaps because it "had run against a stop," limiting its movement."
Isn't the WHOLE purpose of the stop to limit movement? or was the stop jarred loose and was stopping movement when it wasn't supposed to ?
Re:I don't get it ... (Score:4, Informative)
Re:I don't get it ... (Score:5, Funny)
Control Limiting is a Serious Problem (Score:5, Informative)
To summarize the two-day class into one paragraph, a PIO is an oscillation that is generally sustained by pilot inputs, is usually triggered by some external event, and has at least two common causes: rate-limited control actuators, or so-called "phase lags" (lag between input and output).
Relevant to this case, then, is the roll actuator (the hydraulic device responsible for moving the roll control surfaces). It sounds from the non-technical answer in the article "the actuator delayed moving one of the ship's flaps" like a rate-limited actuator. The pilot demanded a larger input faster than the system was able to provide, so the control surface hit its stop.
What ends up happening, in such a case, is that the pilot doesn't get the overall response he expects, so he puts in MORE input. But then it turns out to be too much, so he puts in a response the other way - but it takes a while to start reacting, so he puts in MORE input... etc. etc. etc..
Also, the "external event" in this case was probably a wind shear. You can have a PIO-prone system and it will fly just fine - right up until you hit that trigger event which is just large enough to throw you into a PIO - and then you're basically hosed. Nothing you can physically do will stop the PIO - OTHER than just releasing the controls and letting everything stop naturally - because it's the inputs that drive the oscillation. And you can bet that's quite frightening for a control-freak pilot who's afraid he's about to lose control. Takes a LOT of training in how to recognize it for what it is; stopping it is easy (if you have time or altitude) - just let go.
To fix a control system that has PIO problems, you can (a) increase the authority of the control device, (b) increase the response speed of the device, or (c) decrease the phase lag so it responds more quickly. None of those fixes are trivial, unless they're caused by a broken component.
I'm quite sure Rutan, of all people, is intimately familiar with this issue, and I have no doubt that he and his team will address it appropriately.
Re:Control Limiting is a Serious Problem (Score:3, Interesting)
Knowing a bit about Mike Melvill's attitude, capabilities, skills as a test pilot, and previous flight test responses to unpredicted situations, I think you're barking up the wrong tree with this theory.
The wind shear induced a 90 degree roll to the left, followed by a 90 degree roll to the right. That doesn't sound at all like a pattern of pilot induced oscillation, characterized by overcontrol wi
Re:Control Limiting is a Serious Problem (Score:5, Funny)
I remember an Air Force F-15 pilot telling my father a couple stories about training fighter pilots in some Islamic Persian Gulf state (dunno - I was only 8 years old then). He said the students had an alarming habit of reacting to control difficulties during training flights by letting go of the stick, throwing their arms in the air and shouting "Allahu Akbar". This reaction worked when the trouble was PIO, but he frequently had to take control because the students would simply let go and trust Allah to fly the plane out of trouble for them! One time, shortly before returning to the US, the training aircraft suffered some sort of serious failure and the student pilot shouted "Allahu Akbar" repeatedly as the plane spun out of control. He (the instructor) yelled at him to eject, but he just kept saying "Allahu Akbar". So the instructor ejected and landed without serious injury, while the student rode the plane all the way into the ground.
Good idea (Score:3, Interesting)
And without co-op students, no less! (Score:5, Funny)
Re:And without co-op students, no less! (Score:5, Funny)
Re:And without co-op students, no less! (Score:5, Funny)
According to Scaled's Careers page, "We are sorry but Scaled is unable to hire Summer interns or Co-op students." I didn't think any high tech companies could cope without co-ops and interns!
Huh? They have an intern program. Go to the Jobs section, then look under "Ballast".
Re:And without co-op students, no less! (Score:2, Insightful)
Re:And without co-op students, no less! (Score:5, Funny)
Re:And without co-op students, no less! (Score:2)
Simple Process (Score:4, Funny)
So I guess it's:
1. Fix control surface actuator
2. Fix wind shear problem
3. Profit!
Re:Simple Process (Score:5, Funny)
1. Write code
2. Proclaim success!
3. Prof... err, wait, some bugs
4. Fix code
5. Proclaim success!
6. Prof... err, wait, some bugs
7. Fix code
8. Proclaim success!
9. Prof... err, wait, some bugs
Re:Simple Process (Score:5, Funny)
Re:Simple Process (Score:2, Funny)
Re:Simple Process (Score:2)
Re:Simple Process (Score:5, Interesting)
1. Write code
2. Proclaim success!
3. Prof... err, wait, some bugs
4. Fix code
5. Proclaim success!
6. Prof... err, wait, some bugs
7. Customer or Management changes requirements
8. goto 1.
9. Profit!
Maybe I should debug my development methodology, seeing as I never seem to get to step 9.
The cool thing about the xprize is that it provides a fixed milestone for private companies to shoot for in a fixed timeframe.
I am a big fan of the private 'prize' process, and think that with the success of the xprize we should figure out how to offer a slew of additional prizes to continue to stimulate private space efforts.
I am somewhat surprized that there are not more prizes offered for solutions to hard problems in other areas. Seems like a cheap way for folks to get researchers motivated.
Why not start a non-profit foundation whose sole purpose is to offer bounties with well defined acceptance criteria for a whole range of technical challenges? Any philanthropic and technically oriented billionaires up for the challenge?
Re:Simple Process (Score:5, Interesting)
I think (hope?) that once the X-Prize has been won, there will be another prize put up for the first private flight into orbit, since that's the next big milestone in commercial spaceflight. Or maybe a prize for the first suborbital space flight to the other side of the planet - there are big applications for suborbital space flight as a replacement for normal air travel since once you get our of the atmosphere going hypersonic is much easier.
I must admit that I didn't realise the prize expired at the end of this year though - that kinda puts a lot of pressure on everyone.
Re:Simple Process (Score:2)
See headlines now... (Score:5, Funny)
His luggage lands in Africa somewhere...
Re:See headlines now... (Score:2)
Lighten up people, some jokes I can see getting down modded by mistake or for mentioning proffit or russia, but this one was obviously enough a joke that you'd have to be minus a few clue points to miss.
Mycroft
Re:See headlines now... (Score:5, Funny)
Re:See headlines now... (Score:5, Funny)
Narrator: Was it ticking?
Airport Security Officer: Actually throwers don't worry about ticking 'cause modern bombs don't tick.
Narrator: Sorry, throwers?
Airport Security Officer: Baggage handlers. But, when a suitcase vibrates, then the throwers gotta call the police.
Narrator: My suitcase was vibrating?
Airport Security Officer: Nine times out of ten it's an electric razor, but every once in a while...
[whispering]
Airport Security Officer: it's a dildo. Of course it's company policy never to, imply ownership in the event of a dildo... always use the indefinite article "a dildo", never "your dildo".
Narrator: I don't own...
Passengers (Score:5, Interesting)
Re:Passengers (Score:3, Interesting)
Re:Passengers (Score:3, Interesting)
Re:Passengers (Score:2)
Chaos and Unpredictability (Score:5, Interesting)
I am just quite glad that they had the backup system, because that is what prevented a catastrophy. If there is a x% chance that the primary system will fail, and x% that the backup will fail, combined it makes the chances of a catastrophy much lower.
I believe that if we are going to be successful at a private space race, or even any other high-risk things (Even lacking risk to human life), then redundancy and backup is definitely critical. If a few failed heat tiles can destroy a space craft and kill people, and there is no contingency plan for failed heat tiles, that is a problem. If a computer miscalculation in Metric vs English measurements can completely throw off a multibillion-dollar space probe, and there is no way to recover when the error is first detected and has not yet caused problems, then that is just not right.
I look forward to seeing if they win the prize, and I applaud them for having contingencies. If more systems had contigencies for the most critical failures, we'd possibly be much further ahead in various technologies. Let's see how this space race goes.
Re:Chaos and Unpredictability (Score:2, Interesting)
But I think there is even more to be said for simplicity.
Fortunately both are signature attributes of Burt Rutan.
Re:Chaos and Unpredictability (Score:2)
You mean Metric vs Imperial or American measurements don't you? Here in England we use metric a lot (pretty much 100% of the time in engineering although there's probably a 50:50 split between metric and imperial outside of engineering circles). I honestly couldn't tell you how many yards in a mile, but I know right off the top of my head that there are 1000 metres in a kilometre and that 1 litre of water has a mass of 1 kilogram.
Re:Chaos and Unpredictability (Score:2)
Re:Chaos and Unpredictability (Score:5, Insightful)
The X-prize competitors probably will have SIGNIFICANTLY less redundancy than any NASA craft would ever have (triple redundancy is normal in spaceflight), but they'll also be cheaper, lighter, and faster-to-completion. The associated risks are ones that government-run institutions just wouldn't take.
So, by putting the competition to the public instead of trying to achieve the same thing through NASA/etc. they're able to test riskier technologies quicker and cheaper - resulting in more significant technological advancement.
The risks are great... but they're being taken by individuals that have weighed them and accept them, not a government that's accountable to it's populace.
My meaningless 0.02.
MadCow.
some questions (Score:5, Interesting)
NASA, on some level, is really an organization for several major and minor companies, why would it be ruled out of the prize?
Will commercializing spaceflight be a step forward for space research? Why is it that when companies step into public domain scientific fields the results are inevitably viagra when there is still no cure for cancer, aids... etc. Public grants and public institutions (Nations and Universities) are still the bedrock for pure scientifc research. I only see economic and superficial consumerism inspired by the x-prize.
What do you think?
Re:some questions (Score:5, Interesting)
Because recreational drugs like viagra and alchohol are more valued (practically by definition - they measure this value with their paychecks) by people than the hard-to-make-and-not-very-effective treatments for difficult to cure diseases.
Similarly, Space Tourism has the potential to benefit many many people compared to the handful of astronauts who got to golf on the moon so far.
" Public grants and public institutions (Nations and Universities) are still the bedrock for pure scientifc research. I only see economic and superficial consumerism inspired by the x-prize. "
Public grants fund wierd artwork too. The outcome of both efforts (pure research and wierd artwork) is of direct interest to a pretty small class of people. I'm not saying it's a bad thing; just not wide-reaching.
"NASA, on some level, is really an organization for several major and minor companies, why would it be ruled out of the prize?"
Because NASA is doing it by taking other people's money. If NASA needed 10 more million, they have channels to ask for it. Scaled is doing it with their own.
Re:some questions (Score:3, Interesting)
Viagra is of almost no social benefit. Treatments for cancer save millions of lives around the world each year. Yes they are hard to make (at the moment) and are not always effective and have side effects, but this is exactly why money and effort should be put in this direction. While it may not reap huge economic benefit in the short term, saving lives will help the economies in the long term.
I don't see how pure research is related to "weird artwork". Pure rese
Re:some questions (Score:2, Insightful)
Both contributed a certain number of man-hours-of-happyness to the world. I'd say that's a social benefit.
While it may not reap huge economic benefit in the short term, saving lives will help the economies in the long term.
I bet more healty productive lives were created by Viagra than were saved by cancer drugs. But to me the long term economic benefit seems such a wierd way of measuring the social good of Viagra vs Gemzar I'
Re:some questions (Score:3, Insightful)
When you discover you've got cancer, which are you going to want to buy?
>Space Tourism
Watch the word 'benefit'. Space tourism itself will have little benefit to society, other than to make a few people happy. It's merely a bigger handful than the really small handful of astronauts. The 'benefit' of space tourism to society will be in opening up economy-of-scale for space travel, so that in time we can actually DO something up there. For one, perhaps move enviro
Re:some questions (Score:2, Funny)
Re:some questions (Score:4, Insightful)
Space tourism itself will have little benefit to society, other than to make a few people happy.
On the contrary, space tourism is an excellent way to transfer money out of the hands of those rich enough to afford it and pump it into the economy. It's like a voluntary tax! If this industry takes off it could create many new jobs, technical jobs like we slashdotters like, here on our shores. How exactly is this a problem?
Besides, we (virtually) don't get a say in it, anyway. Frankly, people have the right to spend their money on what they want to. If they want to blow $20 mil on a few moments in space, that's their prerogative. If an insanely rich person wants to fund expeditions into space with new equipment in addition to what NASA is already doing, it's his money, and what could be wrong with that? If you saved for something you really wanted that was expensive, how would you like it if suddenly the world was trying to tell you what you were spending was a waste?
I'd rather see that money go to NASA than many of the things it does go to.
I'm sure both NASA and the SpaceShipOne project would happily accept any private donations you have to offer, if you believe in it that much.
Re:some questions (Score:2)
1. Identify impotence as a problem
2. ??? (i.e. R &: D, and manufacture Viagra)
3. Profit!!!! 4. Once you're bored of making loads of money off viagra, and you've got loads of competitors and are lying in oodles of money, devote your attention to fixing some of the world's real problems, like AIDS, cancer, and George Bush.
Will comme
Re:some questions (Score:3, Informative)
Actually, you are doing Pfizer somewhat of a disservice here. They were actually looking into drugs to be used during heart surgery, specifically drugs to be used to lower blood pressure during same.
During some trials an interesting side effect was noticed. I expect there were some happy happy people.
FYI & FWIW For those interested, high blood pressure is often a cause of impotence (though many might incorrectly argue that a higher pressure might be useful!). Of cour
Re:some questions (Score:2)
Re:some questions (Score:2, Insightful)
This is why it's so distressing that the research aspect of major universities has recently been driven more and more toward economic gain. Presidents and boards a
NASA is ruled out. (Score:2, Interesting)
Yes, Paul Allen paid a lot for this. He paid $20M. But as Rutan (I believe Dick) said at the SSOne launch, Paul Allen could have bought a flight to the ISS with that money (Tito paid $10M), but instead he bought an entire space program. So others will be able to go to space (for short periods) for a whole lot less than t
Re:NASA is ruled out. (Score:2)
Re:some questions (Score:2, Interesting)
Re:some questions (Score:3, Informative)
Cancer and aids research is ongoing. It hasn't stopped. But it's a tough nut to crack, o
Re:some questions (Score:2)
If I'm not mistaken, Viagra was originally a blood pressure drug. Do you really believe that the major durg companies aren't spending millions every year on cancer, aids, etc.? Obviously, they are. It may not be for the altruistic reasons we would like them to, but they are. L
Re:some questions (Score:5, Informative)
NASA was started to consolidate flight research centers. They were scattered in several agencies, although the NCA, widely considered the predecessor to NASA, did operate many of them. With the importation of V-2 rockets from Germany (with a little help from the U.S. Amry going in and taking the rockets by force) rocket research really started to get into high gear. This is where the term "rocket scientist" really came into its own, because before that a rocket scientist was a crazy lunatic like Goddard or Oberth who loved to blow things up.
Both the U.S. Navy and the U.S. Army got into a competition (not with Russia, but with each other) trying to see who could develop these rockets first and claim supremacy on their use. This was no different than what these two military branches did with aircraft just a mere 20 years earlier, including several officers who were involved with the early testing of military aircraft. Both the Navy and the Army Air Corp (later reorganized as the U.S. Air Force) launched thousands of rockets, learning quite a bit regarding how to build them, how to handle them, and what they really could be used for (in addition to putting a nuke on the top of them... that was obvious even to Hitler during WWII).
Later on, particularly after Sputnik achieved orbit, the Eisenhower Administration looked around and saw three competing space programs in the U.S. government. That was the Army, Navy, and a very anemic NCA which was a civilian program. What happened was a transfer of many of the people involved with the Army and Navy programs to the NCA, which was then renamed to become NASA. The parallels with what happened after 9/11 to form the TSA and the Dept. of Homeland Security can compared to how NASA was formed, and this is almost typical knee jerk reaction by Congress.
Because most of the working rocketry projects were already military, NASA took on a military flavor. And of course since many NASA personnel still had connections to the military, those people involved still tried to push goals that would benefit their respective armed services for weapons research. It paid off with the missile programs that are still maintained by the Air Force and Navy, which I guess was your "thinly veiled military control of the program".
NASA was concieved as a civilian-run agency from the beginning because it was obvious to everybody involved that spaceflight would take on aspects that were clearly non-military as well. In addition to trying to sell the program to the American people by trying to give ordinary citizens a "stake" in the program, there was an implied concept that commercial interests would also get involved. AT&T built one of the first commercial satellites (Telestar) and even paid for the whole thing out of their own pocket, including the rocket construction and the salaries of most of the ground crew (by contract through NASA) to get the thing up into space. What happened to kill the Telestar program should speak volumes for what was to come from NASA and is still an issue today.
The big push to seriously expand NASA occured during the Kennedy administration, where JFK was litterally reading some science fiction books, and got a sort of stary-eyed vision about where NASA could go. It was entirely his idea to get astronauts to the moon, and to push for NASA to become even more under civilian control. This was when the second batch of astronauts was announced, and included for the first time civilians like Neil Armstrong who did not hold military rank.
Regarding Columbia: You are doing a huge disservice to the memory of those astronauts to even repeat a wild rumor that has no basis in fact. While there are many things I can complain about regarding how NASA dealt with Columbia, it was not an intentional and deliberate action to kill astronauts. If that were the case, there would be no astronaut corp left at NASA, and they more than anybody else would know more about those issues than any tin-hat conspiracy
Space age (Score:3, Interesting)
Great, but... (Score:3, Interesting)
When they manage to get to 3 times that altitude, then its time to be impressed.
Re:Great, but... (Score:5, Insightful)
Even if that's not enough to impress you, it certainly fills me with amazement.
Spaceship One isn't even a space ship (Score:2, Interesting)
Re:Spaceship One isn't even a space ship (Score:3, Insightful)
Re:Spaceship One isn't even a space ship (Score:3, Insightful)
The whole point of the X-prize competition is to encourage the development of rocket vehicles that would be capable of spaceflight, and you have to start somewhere. The X-prize tried to set a goal high enough that it would be difficult to obtain (many thought it was impossible for people to do this on their own dime) but yet easy enough that private
Re:Spaceship One isn't even a space ship (Score:2)
Indeed , and because of that its a very laudable endeavour. My point is simply that Spaceship One is not (yet) a spaceship. One day it or its descendents probably will be but its just premature to call it one now. The mans achievement is impressive but I do get the feeling that he's claiming he's running before he's really even walked. Though as usual on slashdot if you're
Re:Spaceship One isn't even a space ship (Score:2)
Re:Spaceship One isn't even a space ship (Score:3, Interesting)
It has maneuvering thrusters, it has an O2 cannister because they have to carry their oxygen somehow. The cabin is pressurized however. If it were a bigger ship on a longer mission, of course it would be different. And finally, reentry. We've been re-entering the earth at breakneck speeds because it's the simplest physically (although not technically). Who's to say it's right? If someone can design a ship that can slow
Re:Spaceship One isn't even a space ship (Score:2)
Is it? Well in that case they won't need to modify it at all to into orbit will they? Whats that? It can't do it? But you just said its a proper spacecraft. So its a spacecraft that can't stay in space. Make your mind up.
Re:Spaceship One isn't even a space ship (Score:2)
What is your definition of a spacecraft? Would not being able to enter and exit space be the main requirement? By all acounts, staying in space is among the easie
Re:Spaceship One isn't even a space ship (Score:2)
As far as re-entry, there's nothing to prevent future shuttle type craft from taking an example from this and taking the time to slow down so it doesn't fall apart during re-entry. Thats one of the things that has some people excited. It hasn't really been done before, and they've shown that if you re-enter slow enough there's no problems with overheating. Some people are
Re:Spaceship One isn't even a space ship (Score:2)
Re:Spaceship One isn't even a space ship (Score:2)
This is why it is useful.
Re:Spaceship One isn't even a space ship (Score:2)
Re:Spaceship One isn't even a space ship (Score:2)
As mentioned in a previous Slashdot article about Blaise Gassend's Notes from the Third Annual Space Elevator Conference [mit.edu].
Re:Spaceship One isn't even a space ship (Score:4, Interesting)
Not really. The Chinese reportedly used thick sheets of (admittedly chemically treated) oak on some of their early unmanned launches.
"The protective tiles on the Space Shuttle, for example, are expensive, and very fragile."
I think it's a safe bet that Rutan won't be using such tiles on SpaceShipTwo.
"Ablative heatshields are a possibility, but they do add to the per flight cost."
A properly designed ablative heatshield is much easier to remove and replace than shuttle tiles are to maintain. You just unbolt the old one, slap on the new one and you're ready to go... with tiles you have to check they're all in place, check they're all secure, and make sure there are no bumps larger than about a millimeter over the entire underside. That's a huge job, and one of the reasons why the shuttle takes so long to turn around.
(Note: ablative shields weren't really an option for the shuttle as designed, but there were a lot of other designs proposed before this one was picked).
An intriguing way to protect during descent. (Score:4, Interesting)
Why not? Cryrogenic fuels are extremely cold, and it is theoretically possible to route these cryrogenic fuels to actually cool down the spacecraft's structure during atmospheric re-entry if there is a safe way to vent the heated fuel. When Douglas Aircraft did its studies for the ROMBUS launch system in the early 1960's they actually figured out a way to use liquid hydrogen to provide heat protection during the descent. I'm sure that Burt Rutan knows about this idea and might use something like liquid methane as a rocket fuel for the ascent and as a coolant to protect the structure on Scaled Composites' Tier Two/SpaceShipTwo project.
Re:Great, but... (Score:5, Insightful)
The prize is for Manned Flight.
Speaking of which, isn't "Space Flight" an oxymoron? Flight implies flying, movement through a medium using lift mechanisms. I was under the impression that generating lift required a medium a little more dense than the vacuum of space. Anyways... I don't see your Sub-Orbital Rocket Plane or Missile on the X-Prize list of contenders.. so that makes you:
a hater, don't hate.
Re:Great, but... (Score:2)
Re:Great, but... (Score:2)
They will have to fly twice to win the X-Prize. (Score:4, Interesting)
It's an important detail, because it means the vehicles have to be reusable with minimal refitting.
The Space Shuttle could never win the X-Prize, even if it were flying and qualified for the contest, because its turnaround time is too long.
Jon Acheson
175 days left to win prize (Score:3, Insightful)
Re:175 days left to win prize (Score:3, Informative)
This is why there is a time limit. It wasn't there originally, but once there were
Re:Wind Shear (Score:5, Insightful)
Re:Wind Shear (Score:5, Interesting)
Re:Wind Shear (Score:3, Interesting)
2) The sub-zero temperature O-ring failure issue was indeed NASA's fault (Statistics rule #1: Never omit data (in this case, omitting successes and simply plotting failures) to simplify a graph.). However you can pick on anything from an organization that has launched tens of thousands of rockets of hundreds of designs.
Rutan didn't do one of the most basic things in spacecraft launch (don't launch in high wind
Re:Wind Shear (Score:5, Funny)
Me first thing I worry about is the Huge laser cannons and force shields. That and a seat for cute blue space chick.
Maybe this is why NASA hasn't called back.
Mycroft
Re:Wind Shear (Score:5, Interesting)
The deal with wind shear is this. Ordinarily, airplanes move within moving masses of air and get carried along by them. This is no big deal except that it affects navigation (e.g., even though your nose is pointed north, you might really be tracking northeast because you are within a mass of air moving from west to east). Moving masses of air don't ordinarly affect the airplane in an "aerodynamic" sense because what matters is how the plane is moving relative to that mass of air, not relative to the ground. Wind shear occurs because there are often distinct boundaries between different masses of air that are moving in different directions or at different speeds. Hitting a wind shear boundary can be an issue because due to inertia (or momentum, whatever you prefer to call it), the plane does not instantly make the transition to the new conditions, so its situation changes temporarily relative to the air. But it's only scary when the extent of the change is greater than the aerodynamic limits for your airplane and your present attitude.
For example, if you are flying at just five knots above stall speed, and you hit a boundary that has an abrupt ten knot difference in the wrong direction, it can pull the rug out from under you. But if you're flying at normal cruising speed, that same difference just causes a little turbulence. So to have a critical problem with wind shear you need both factors -- being near one of your aerodynamic limits (stall speed, red line, whatever) PLUS hitting a boundary that emphasizes the change in air movement in the WRONG direction for that limit.
So the reason I am skeptical is that Rutan gives no explanation for how exactly wind shear caused the loss of control. Was the ship being operated near its stall speed? Was the wind shear differential totally huge? Was the ship in a weird attitude (high bank angle or something) that reduced its tolerance to changes in airspeed? And is there any meteorologic evidence of any big wind shear conditions at that place and time? Otherwise, it is just wishful thinking that he has an explanation for this?
Re:Wind Shear (Score:2)
Only thing I can think of is if the two wings were in differently moving masses of air when this occured. He was likely travelling very fast at the time, near his top speed (mach3? my memory is crap today).
Mycroft
Re:Wind Shear (Score:5, Informative)
So I would tend to believe the wind shear explanation:
At the start of the climb, the "plane" (more like a winged rocket, really) had high thrust but low speed, went vertical and hit wind shear. Each wing was going through a different wing mass, and this spun the plane 90 degrees. After that, the plane was going fast enough that wind shear didn't matter.
Incidentally, I was there watching with another 20,000+ people. It was impressive, seeing this white streak shooting vertically.
Re:Wind Shear (Score:2)
Wish I had the option of being there, but I live in the St. Louis are of Missouri, a little far for a weekend drive.
Mycroft
Re:Wind Shear (Score:5, Interesting)
Your explanation sounds great, but, you are using the wrong frame of reference. You are considering classic wind shear at low level/low speed accident scenarios, because that's what the schools teach about. Finding a shear greater than 20 knots at low level is rare indeed. Head up to the tropopause, and it's a totally different story.
At the junction between troposphere and stratosphere is this little phenomena known as the 'jet stream'. 100 knots of shear on the boundary of the jet streams is actually 'quite normal' and 'not bad'. I've seen 150 knots of shear over a very short distance vertically (less than 2000 feet) while penetrating the jets. This is still not a huge big deal, just gets a little bumpy, but, take a good look at SS1.
At the time of the roll event, the aircraft was accelerating on the initial rocket boost. It was in transonic, or early supersonic flight regimes. Penetrating a shear layer that gives a 100 knot difference in relative airspeed would set up some very very interesting asymetric shock wave scenarios, where the shock buildup on one side of the airframe is completely different than on the other. Even if this situation is just momentary, the asymetric forces will be huge, and cause a very noticeable deviation from nominal flight path projections.
Your frame of reference for shear is 'low and slow' in 'low performance' aircraft. SS1 is a very high performance aircraft, operating 'high and fast'. The primary contributor to aerodymanic forces will be shock waves and various forms of drag they produce. It's a whole different world, and everything you learned about 'low and slow' just doesn't apply to the 'high and fast' flight regimes. The SS1 flight mode at the time of the upset was 'at or near vertical' at transonic or supersonic speeds. It would not be at all surprising to see a major upset in the craft stability if it accidently penetrated the core of a 150 knot jet during that flight condition.
At this time of year, at those lattitudes, the core of the jets would be at an altitude in the area of 45 to 55 thousand feet. It would be unusual to see a jet core that far south in June, but, not unheard of. It's to late, and i'm really not inclined to go dig up old met charts from a couple weeks back, and see what kind of jet stream cores were over that part of california that morning. Sounds to me like that's what they may have hit, and, means the meteorology guys will be watching the jet charts a LOT closer for the next launches. Wouldn't surprise me at all that they even overlooked the detail, with an attitude of 'jet stream cores, over california, in june, who are you trying to kid?'. It's common in the winter, but not in the summer.
Re:Wind Shear (Score:3, Informative)
The kind of turbulence of which you speak can have very drastic affects on an airframe. Particularly if the turbulence is generated by something heavy flying slowly and you are in something light. They will teach you in class to stay above and well behind anything heavy and slow in front of you. Note that slow for them may be in excess of your maximum attainable speed in level flight!
In other words, its certainly a real issue, but any turbulence encountered by SS1 was not due to turbulence from other cr
Re:another trip == couns:? (Score:2)
Mycroft
Re:another trip == couns:? (Score:5, Informative)
Re:dont-run-away.-Stay-on-earth (Score:3, Interesting)
I agree... it would indeed be sad to see Spaceship-One go into a hanger and never come out again, except for a trip to the smithsonian 30 years later.
Of course, I really want to see a successful X-prize flight, followed by a series of private companies getting in line to order their own spacecraft from Scaled Composites.
NASA would make a very smart move by buying a couple of these and using them for actual routine space-flights. Of course, my intuition tells me that NAS