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+1 to your thoughts Jeff, well said.
I have 20+ years working in commercial aviation as well, and I have never met an engineer who would cut a corner relating to safety in any reckless way. The standard I work to and the standard of all those I have worked with is "would you fly your familly on it". This is the level we always work too.... Arm chair quarter backing is fun for those that know nothing and risk nothing....These people are exploring space for passion and knowledge...do you honestly think this is the highest ROI branson could achieve with this kind of investment? No he does it because he loves aviation, and development that reduces the costs of space travel is very much moving forward technologically. |
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I've done my share of flying, still not a comfortable experience. Great points made by Jeff and gordner about safety and family. |
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That said, I see this effort as so far away (lagging) from the efforts of the likes of Boeing. Essentially, the SS1 / SS2 teams have been working hard on a cheap way to touch space. --and they did touch space with SS1. From Burt Rutan 2003; " Safety, of course is paramount, but minimum cost is critical. " per Scaled Composites: SpaceShipOne All of these types of ventures are a balance between risk vs cost. There is that saying about life - it's a balance between risk and boredom. The people at Scaled/Virgin made decisions about that balance. So, while I agree that it's stupid to MMQB that these people shouldn't have taken risk, the spectacular failure points to a very high likelihood of cutting one too many corner. --what that is, I would really like to know. For me, and my experience with carbon-fiber clad aramid honeycomb, I look at that wreckage and see far too fragile of a structure for handling that much energy. Of course I have nothing quantitative. Maybe the failure will prove to be something completely unrelated; but still, for my personal risk assessment, you couldn't pay me to go super-sonic in that craft. OTOH, I would jump at a chance to ride in a 50 year old tech SR-71. |
Looks like pilot error in this case. Something that can happen to any vehicle regardless of when or how it was made.
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What happened? Did he fly it into a tree?
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Speaking of stability, there is this from Wikipedia: Quote:
Also note, that the highest (design) G-loading (6g) is when feathered and hitting the atmosphere at ~Mach4 -- it was moving at ~Mach1 when this anomaly happened. --Maybe Mach-tuck produced enough moment on the body to overcome the feather.. . meh That doesn't add up, in my lil brain. Well, other than the people with the supersonic shuttlecock want to reassure the hell out of believers that everything is solid as a rock . ..unless something goes wrong - then it's Pioneering new technology. ...and pilot error. Perhaps the politics of protecting manufactured narrative have begun. :-/ |
Perhaps if you don't understand the dynamics of the situation you should go read up on aerodynamics. Plus, he didn't pull the release a couple seconds early. He pulled it a couple minutes early.
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It has been a couple decades since my applied aerodynamics engineering - and that was mostly for my interest in turbomachinery. Feel free to set me straight. :) |
It has been a couple decades for me as well, but anyone that has had about any engineering course can tell when you have that much deflection at that altitude it is going to stress the airframe beyond the design limits. Just like the plane Geoffry DeHaviland (sp?) crashed. Or the M21 with far less deflection, albeit at a higher speed.
Far different situation than coming down from 100km at speed or going out of control at a slow speed glide. |
Deflection? Of the structure? Or are you suggesting a sudden change in angle of attack, due to the release of the feather lockout? --I'll assume the later.
The center of drag, of the feathers, is well above and behind the pivot point. So how does this induce a change to the angle of attack? Also of note, it has been stated that the feathers need to be driven upward. |
Watch this video if you don't understand how it works.
<iframe width="640" height="360" src="//www.youtube.com/embed/Lqhzlq7UReA?feature=player_detailpage" frameborder="0" allowfullscreen></iframe> |
Nice glide. Speed?
Here, at 38 seconds, and under rocket power, the pilot calls unlock. (feathers go up during glide.) <iframe width="1280" height="720" src="//www.youtube.com/embed/H-khULLjtgU" frameborder="0" allowfullscreen></iframe> |
Now lets talk about a Mach plus ejection survival!
I think there is only one case of a non-pressurized cabin non-protection capsule mach plus ejection survival I think of a weekend warrior in an F-15 off of the east coast that survived I think. I would say not knowing this ship, that the pilots survival was something!
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Those that witnessed it said that the craft dropped from the support vehicle the way it was designed to and when it had fallen far enough below it, the engine fired off for very few seconds (not the pre-planned length of time required to take it to the prescribed altitude), then stopped prematurely. Then it fired up again and promptly exploded. I'm not sure when the feathering occurred, but the way I heard it, it wasn't that the copilot feathered it "a couple seconds early" it was that the engine malfunctioned. Maybe the malfunction procedure is to feather it at some point to bring it back once some kind of shutdown procedure is concluded. I don't know if there is any "help" in these videos... http://forums.pelicanparts.com/off-topic-discussions/836586-virgin-galactic-spaceship-crashes-4.html#post8337560 |
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From NTSB
Hart: Review of cockpit forward looking camera shows that the feather was unlocked by the copilot. #SpaceShipTwo Hart: Normal procedures are to unlock feathers after Mach 1.4 so aerodynamic forces do not extend feathers prematurely. #SpaceShipTwo Hart: Engine burn was nominal up until feather extension. #SpaceShipTwo |
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Here is a similar story from decades past. (Mach survival, unstart..) Quote:
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http://forums.pelicanparts.com/uploa...1415296220.jpg |
FWIW, I have read that the reason the new fuel was being tested was due to the mothership not being able to reach the design release alt of 50,000 ft. (therefore the SS2 rocket needs to make up the difference)
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