Certainly looks like a stall...
...but the video only shows the very end of the action.
I found a longer video:
https://www.youtube.com/watch?v=Z5Slv6E5ntQ
Clearly it's not a true stall. Seems like they lost control for some other reason.
The Airlander 10 hybrid – part airplane and part airship – has had a bumpy touchdown after piling into its landing site nose first. The 92-meter (302-foot) aircraft gets 60 per cent of its lift from the helium that fills its two massive airbags, which have earned the aircraft its nickname of the Flying Bum, although the …
...but the video only shows the very end of the action.
I found a longer video:
https://www.youtube.com/watch?v=Z5Slv6E5ntQ
Clearly it's not a true stall. Seems like they lost control for some other reason.
I suspect that the pilot may not have appreciated just how severe the nose-down attitude was
Are you sure? Got no airship piloting experience to draw on; but I would have thought that being strapped into a shed on the bottom of that thing would give you an immensely detailed appreciation of angles. Aside from anything else, he would have started spilling tea once it went past about 15 degrees off horizontal.
It doesn't really look like a stall at all - in the longer vid, linked above, the Airlander is already in a nose-down attitude before the final pitch-down. Also, if you full-screen the higher res video in the Reg article, you can see a grounding line hanging below the rear of the control cabin but it doesn't appear to get snagged; it just seems to drop vertically until just before touch-down.
What appears to happen is that the front ducted fans continue to be vectored backwards along the axis of the craft while it's descending, driving it downwards. Then, when it's clear that the attitude is too extreme, the fans start to be vectored downwards but not by nearly enough - they are still largely pointing backwards along the axis and continue driving the craft downwards.
I doubt that the fans are that restricted in their vectoring limits so I suspect that the pilot may not have appreciated just how severe the nose-down attitude was and so just didn't vector the fans enough: Controlled Flight into Terrain.
I'll be interested to read the AAIB report when it's out.
@LeeE:
I doubt that the fans are that restricted in their vectoring limits
I believe (and this info is very difficult to pin down) the forward propulsors are limited in swivelling to +-20 degrees. But additional thrust vectoring is available through using the movable vanes in the propwash. It's very difficult to impossible to judge the final vector direction by inspection.
"I believe (and this info is very difficult to pin down) the forward propulsors are limited in swivelling to +-20 degrees."
I don't know what the vectoring limits are but as the Airlander is designed to operate in (slightly) heavier-than-air mode I'd be very surprised if the fans can't be vectored directly downwards to help compensate for varying loads whilst taking-off and landing. In fact, if you're going to fit vectoring fans on a craft of this type, I'd be a bit surprised if they can't be vectored in any direction, especially directly forwards, to aid braking and positioning.
If you're going to fit vectoring fans I just can't see any good reason for limiting the vector range at all unless the designers only stressed the fan mountings for that +/- 20 deg range, which would seem to be either a bit of an oversight or an indication of marginal performance (in some respect) that could only be addressed by limiting the stress capability of the fan mountings.
If the fans are limited to just +/- 20 deg, I'd be very curious to know exactly why because given the entire context i.e. not just the type and design of the craft, but also its originating customer and intended purpose (military), those limits just don't seem to make much sense.
I don't think you can stall a wing at near zero airspeed, though maybe they were into wind and the breeze dropped suddenly. Or a breeze picked up and aerodynamically caused the pitch down. I could imagine that being such a big area, once the nose is pitched down into wind then they would be fighting a very large aerodynamic force trying to force it down more.
It looked like the rotating engine pods at the front weren't capable of turning directing much downward thrust that could have helped level the thing.
Sitting in that cockpit would have felt like they were going in at a much steeper angle than it looked from outside. At least, though, all they need to do to repair is to bolt another shed on the bottom. Maybe attach a couple of straw bales to it next time though.
'I don't think you can stall a wing at near zero airspeed'
Pedantically wings stall at an angle of attack, specifically the one where the flow separates from the upper surface. It's just easier for pilots to use the airspeed this happens at as it's actually displayed in the cockpit. However that airspeed will change with all up mass and g-force.
"At least, though, all they need to do to repair is to bolt another shed on the bottom. Maybe attach a couple of straw bales to it next time though."
Maybe in the next iteration, put the shed on the top and all soft bouncy stuff on the bottom. Just in case, like.
"They should have pumped ballast to the rear of the ship....." An interesting idea - maybe it was a ballast issue, but also a control issue in that they accidentally pumped water ballast forward in a panic when they should have pumped it aft. Some flying accidents are caused by the pilot being twisted round to look aft and then moving the controls the wrong way, then compounding the problem by pushing the controls even more the wrong way in panic. It would explain how the dive seemed to continue to steepen rather than starting to recover.
Admittedly I don't know the details of this particular ship but I have flown on an Airship Industries Skyship 500 and the pilot assured me that all the other airships he had flown used ballast to change the pitch attitude. Not surprisingly they use air, not water, as they don't need to carry it around with them when it not needed. Basically, there is a large bladder at each end, with a very big fan pushing air in when required. This has 2 effects:-
1) air is surprisingly heavy when you have enough of it (or light in a hot air balloon)
2) the volume occupied by the by the bladder pushes on the helium balloon thus reducing the lift at that end of the ship.
I was slightly surprised when he showed me the bladder evacuation system which consisted of a rope and pulley which lifted a big flap and let the air out again. Simple but effective. On the Skyship, the pilot achieved 30° of pitch up which I think was mainly due to the bladders since it has no aerofoils.
As someone on Slashdot pointed out. This thing need 38,000 cubic metres of helium to operate. Yeah, that stuff that's rare, almost impossible to create, used for vital things like science and medicine.
And they want to build ten, and larger versions? The helium costs alone would become prohibitive over time, and there's a lot better things you could be doing with it than having the world's slowest crash in a giant ass-shape balloon.
That's not entirely true.
Until recently there was no point conducting helium mining exploration because the US were artificially depressing the price by running down their massive stockpile.
Now that's almost exhausted, exploration has begun. And quite successfully too http://www.bbc.com/news/science-environment-36651048
Helium is relatively easy to create. It is a by-product in the manufacture of tritium, and a waste product of experimental fusion reactors. Manufacturing elements is expensive and only worth the trouble if the element does not exist naturally and has a profitable / military use. Even collecting naturally occurring Helium is not worth the effort - unless someone creates a market for it by, for example, flying giant airships.
Helium production by that means would be ridiculously expensive. Helium currently produced is a byproduct of natural gas production - over geological time enough has accumulated from captured alpha particles that it can be (just barely) profitable to purify and ship it.
Actually mostly found being bled off oil wells in Texas. And IIRC the US is selling it's entire strategic reserve (about 1 billion cubic metres) on the open market because they did not need that much for err strategic uses.
It''s been along time since I thought the only way you could get He was distilling air.
It's not.
Yeah, that stuff that's rare, almost impossible to create, used for vital things like science and medicine.
Earth's atmosphere has 3.77x10^12kg of helium, enough to fill 555 million Airlanders. And if they spring a leak it goes back in the atmosphere.
Helium production by fractional distillation of air isn't cost effective when the competing source is sticking a fancy steel straw in the ground, but it's not rare.
@cray74:
Well, all neon is produced by fractional distillation of atmospheric air. However, it costs $330/kg. The volumetric concentration of helium in the atmosphere, however, is less than one third that of neon, so it would be extremely expensive to produce using this method. Logic would suggest at least $3000/kg (the density being 1/3 as much as neon in addition to the concentration being 1/3 as much).
Right now, helium extracted from natural gas costs only in the general neighborhood of $20-30/kg.
Suggestion for El Reg: Go to Cardington and photograph the hangar...those are sheds on an epic scale that you simply won't believe until you see it. I used to live near there; saw them multiple times and still don't believe it. The Cardington sheds are one of those things that you don't believe while looking at it. Take someone else, so they can be a tiny dot in front of the doors for perspective.
Sheds as landscape. If you can make those invisible, I'll be genuinely impressed.
Recently visited the ex CargoLifter hangar in eadt Germany (now a tropical swimming pool/resort). The scale of these buildings is just mindboggling. You feel truly tiny standing under something that big. (The cargolifter hall could contain the eiffel towe on its side. With room to spare)
CargoLifter was btw also the previous company to try this exact idea. They built the hangar and promptly ran out of money.
Indeed, they are ENORMOUS.. I live and work just around the corner from them (got to see the flying bum yesterday as well from the office). Even when you're standing right next to them, the scale of them still doesn't compute.. incredible buildings, and look fantastic after their refurbishment too.
To be fair, it must have been pretty scary for the pilots, stuck out in the gondola with the ground, slowly, slowly, coming, right, at, them.
The suspense would make it worse.
(and looking at the 'after' photos, it might have looked soft, but it smashed up the cabin pretty well.)
"....it might have looked soft, but it smashed up the cabin pretty well.)" True, but a conventional aircraft nosing in from that height would probably have left a smoking crater! One of my relatives had a great story from 1940 about how his experienced CO, Squadron Leader Hurll Chester, wrote off a Blenheim bomber at zero feet and zero knots! After landing at Upwood, he meant to select flaps UP (standard procedure when parking the Blenheim), but accidentally selected gear UP - the resulting damage was severe enough the airframe was written off and used for ground instructional purposes!
... earlier in Germany? I seem to recall that there was this Cargolifter company, and they planned an airship with the capacity for 160000 kg (or some outrageous number). Money was burnt - mostly small investors, if I recall correctly. The hangar now houses a "tropical" wellness / swim thing. It is also a nice navigational landmark ;)
I liked the idea, though.
Quick google didn't take you to wiki?
"Named the Martha Gwyn after the company chairman's wife"
Admittedly, the source for this is the Daily Fail, but I'm not going to link to that rag, but the Chairman of Hybrid AirVehicles is Philip Gwyn (according to their wiki, and I'm too lazy to check further)
"Named the Martha Gwyn after the company chairman's wife"
Martha Gwyn: "You've named your airship after me? Oh how sweet! Is it becouse you love me Darling?
Philip Gwyn: "Nah love. It's becouse you're slow, have your head in the clouds most of the time, and your arse is so massive you can't sit down without crushing something..."
<SLAP>
Airship vs fixed wing "It`s an entirely different type of flying altogether"
Not exactly entirely different. The physical realities governing airship flight are a superset of those governing fixed-wing flight. Both have aerodynamic influences following the same physics, and to these the airship adds aerostatic influences.
Both can blunder into the ground.
Thus demonstrating the real problem with airships (as opposed to the ones "everyone knows"), the problem that killed so many in the Glory Days of the Dirigible: when you have a bouyancy mechanism providing the lift that relies on having lifting masses of gas very far apart, local changes in air density can kill you faster than you can yell "release ballast aft!" as a machine longer than however many sperm whales laid nose-to-tail flies into a pocket of air denser than that in which the tail of the craft is currently situated.
Shortly after this the poorly-named aerostat will nose-stand and the crew will individually release ballast aft.
Unless the ground gets in the way first.
The main aim of this design is to solve that problem. It's not a purely helium-lift - it has ducted fans too. Without those it's actually just a little heavier than air. The fans can respond very quickly in order to maintain attitude.
That's the idea, anyway. Looks like they still need to work a few bugs out.
Hasn't anyone thought to blame it on a Welsh drone pilot yet?
"Get ready for landing! Switch off the anti-crash software!"
.............."Oh crap!"..............GRRRIIIINNNDDD!