Armadillo Aero One Step Closer To Space
RobertB-DC writes "The folks at Armadillo Aerospace have taken another step toward the X-Prize, dropping their re-entry vehicle from 2000 feet with no major problems noted. As usual, the Armadillo crew documented the event with text, pictures and video, and the story is also covered by Space.com (though without as many cool technical details). It's a bumpy ride, though -- instruments recorded some 10 G's on touchdown."
Were their inertion dampening fields down?
Perhaps they dropped their server from 2000 feet also!
Now they're getting somewhere. John Carmack finally quit trying to win the prize by running at brick walls and firing a Stinger missile at the ground.
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I'm not sure how much it costs to put this thing up. But, at 10 G's per touchdown, a bunch of more of these and they may get close to breaking even!
It could be a very smooth, fast drop.
Lately, we've been hearing more and more about the X Prize and the amateur (and not-so-amateur) aerospace engineers taking part.
/might/ be different, but the goals are the same: Take something that you can't have general access to, make it your own, and make it better. Then contribute that idea to the general public.
I suspect that the recent projects are to the government-sponsored space programs as open source software is to commercial software. True, the fundamental ideas
In an era when people are becoming more and more concerned with manned space flight, I think projects and contests like this are the only way possible to get humanity into the heavens. Governments will always be under pressure to reduce spending; it will only be with enthusiasts that we make it to our proper place in space.
(This isn't to say, of course, that a non-government-sponsored flight will be the first to Mars. This is simply to say that it will be the space enthusiasts who shed the light on the important facts about space and its wealth of knowledge.)
From the website:
Too many users... blah blah blah
Probable cause: http://www.slashdot.org
Try again in a few seconds...
-xian@idsoftware.com
Is armadilloaerospace.com already down?
Here's the google cache
This links right to the video and the pics are here
http://www.armadilloaerospace.com/n.x/Armadillo/Ho me/Widget`s Corner?news_id=214
We finished up all of the prep work for the vehicle on Tuesday. We welded in strapping points to hold 600 pounds of passenger sandbags in the cabin area, and we mounted five 45 pound Olympic barbell plates on a peg at the end to simulate the weight of the final engines, plumbing, and backup recovery system that will be on the full size vehicle. We mounted four 2 throat engine shells as placeholders. Total weight is just under 2400 pounds. We use a combination of multiple chain hoists, a palette jack, and a forklift to move the full vehicle around and get it up on the trailer, but we did wind up breaking one of the castor wheels that we had mounted on our tank cradle. If we wind up having to use the 1600 gallon propellant tank (the current one is 850 gallons), we arent going to be able to stand the vehicle up under the main girder inside our shop, which will be inconvenient.
On Saturday, we headed out to our test site for the drop test. There were quite a few stares on the road in transit We had a few spatters of rain, and the wind occasionally gusted to 12 knots, but we were able to perform the drop in relatively calm 6 knot winds.
Anna rented a big RV for the day, which was very worthwhile. It was nice to be able to take a break in an air-conditioned space.
5 State Helicopters arrived with a big Sikorsky for the lifting. It was very convenient that they were based close by, and didnt have a problem with our unusual application (although they did have us contact the local mayor and sheriff for explicit permission). We were very impressed with the precision that they were able to do the lifting we were afraid that the vehicle might get dragged or bounced on the crush cone, which could buckle it before the test even started, but they were able to perfectly pivot it up on the nose, and gently lift it off the ground. If we had known they were that precise, we probably could have skipped renting the forklift truck for recovery and just had them lower the rocket back onto the trailer after the test.
We made several 18 diameter test parachutes that were weighted to drift at about the same rate that the full size parachute was expected to fall. We did the test drop from 1500 AGL, under the assumption that the big vehicle would fall several hundred feet before the main chute was fully deployed. The landing point for the test parachute was satisfactory, so we planned the full vehicle drop for 2000 AGL. Neil rode in the helicopter to do the parachute releasing, and Anna hung out the side of the helicopter (with a safety strap) to get aerial footage.
We had to abort our first attempt to drop the vehicle, because the line that we ran from the helicopter to the Sea-Catch toggle release above the rocket had wrapped itself around the chain so many times that Neil couldnt pull it hard enough to trigger the release. This was fixed by tying loose loops of plastic every few feet along the chain, which kept the pull-line in place.
On the second try, the release worked perfectly. You can clearly see the naturally unstable aerodynamics of the vehicle, as it starts to tip over almost immediately after release. We all held our breath as it started to fall, but the drogue immediately inflated and started pulling the main canopy out. It was nine seconds from release to full canopy inflation. The opening shock was negligible, barely hitting 2Gs. For high altitude flights, we are aiming for a 200 mph terminal velocity under the stabilizer drogue at the time of main canopy deployment, so opening shock will be much greater then.
The wake of the main canopy is so great that the deployment drogue just rests on the canopy during descent, without any inflation at all. The real deployment system will have a much longe
I've seen a dead armadillo, but I've never seen a dead armadillo cooked in rocket fuel. That would be new.
If tits were wings it'd be flying around.
Is the site slashdotted already or did they drop the vehicle on their web server?
Crash rated seats for military helicopters are rated to take 50G down to 20G so I wouldn't think 10G would be a problem to deal with.
Good thing they only recorded some 10 G's. If those 10 G's had been present all over the craft, who knows what kind of complications could have arisen. I'm sure the design team will find a way to spread those 10 G's throughout the craft, reducing the overall readings to a manageable 2 or 3 G's.
..The problem with these people is that their movie clips are waaaay too large. They could reduce their movie file sizes by a factor of 5. I am sure that would alleviate some of the pressure on their server... Has noone pointed this out to them?
Depends on many milliseconds of duration. Humans have been shown to take 35 G's for very short durations (belted head on collision at 50 mph for example), but anything over about a 100 milliseconds and your organs (and bones) tend to go a little mushy.
[RIAA] says its concern is artists. That's true, in just the sense that a cattle rancher is concerned about its cattle.
John Carmack is a semi-regular poster to sci.space.policy on usenet; he's posted several times today with details of his test plans and schedules. Even if the company site is slashdotted, go do a Google Groups search on him and the sci.space.* groups and you'll get all his publically-available info, straight from the source.
Stop playing with those rocket thingys and go finish your job!
It should actually be written "10 g's", with 'g' in lower case, as this refers to 10 times the normal acceleration, while "G" the capital letter refers to something entirely different.
Anyone else think this is wrong? When touching down 10 G's? The most G's would be on lift off, not touch down, and 10 is just plain nuts. Come on. If you think of a plane, and touchdown, you are going in the same direction of gravity, not against it.
I mean conceptually, the article doesn't make sense, and I hope people will realize that.
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Unix is very user friendly, it's just picky about who its friends are.
Visit www.scaled.com and you'll see who's going to win the X-Prize. Burt Rutan designer of the famous Voyager, the plane that made the first non-stop flight around the world.
This guy has been engineering exceptional aircraft for years. Father of one of the most radical and popular homebuilt aircraft designs ever.
J.C. has an interesting background and obviously the mind of an engineer, but no one is going to catch up with Rutan's design which resembles the X-15 project of the 1960's.
If someone at Scaled Composites is reading... Can I have a job? Yeah, like that will happen...
The X prize is about paving the way for paying customers to get to space. It's about developing a cheap re-usable space craft to do it. Lighting off hair chemicals for launches and crashing for landings? You gonna pony up for that? Go ahead. I'll call Rutan for my flight, thanks.
Good Grief. - Charles Brown
That X-15ish engineering may be Scaled's achellies heel. Remember that the well financed front-runner for the Orteig prize crashed the day before Lindberg took off.
I'm hopeing that both teams get their first launch within days of eachother, so that a media frenzy occurs before the winning launch.
RocketForge had a link to this posted 3 days ago! So I got to see the video before you guys slashdotted the server :-)
Energy: time to change the picture.
I choose to base my logic on the movie Armageddon where people can cheerily pull 18 G's on the backside of the moon.... before landing on an asteroid... and blowing it up...
perhaps i need to find a new base for my logic...
It's not stupid. It's advanced.
Yeah, but they are probably in pretty good physical condition. Your average geek gets woozie just bending over to pick up that stray cheese doodle.
BitTorrent of the Video here:
p Test.mpg.mpeg.torrent
http://www.bytemonsoon.com/download.php/11286/Dro
Whenever the offence inspires less horror than the punishment, the rigour of penal law is obliged to give way...
It could be a very smooth, fast drop.
As the old saying goes about leaping off a bridge, it's not the trip down that sucks- it's the ending.
The joke among some pilots, after a hard landing, is the term "unintentional ground contact."
Please help metamoderate.
seems like a lot of trouble to squach an armadillo. Usually speeding cars do just fine.
"dope will get you through times of no money better than money will get you through times of no dope"
"10Gs" isn't really that informative. In addition to meters per second squared, the key units to report for the landing are meters per second cubed or "jerk". That tells you how much destructive load is imparted by the acceleration. If they published the accelerometer output it should be easy to figure.
Seastead this.
I keep seeing people quote those high g numbers from historic tests of days past. One of the most critical factors in determining how fatal a g rating is on a human, is not only the g's, but the duration the g's were sustained. For example, a human can take insanely high g's over a very finite duration. Those same g's which may of only bruised and bloodied your body may have killed you if the same g's were sustained for twice the duration.
Others are simply pie-in-the-sky.
Rutan is trying to do things in the hardest way possible and you know what that means... However there are rumours there could be a possible government money source behind this interest by Rutan. Remains to be seen.
BTW a suborbital flight is nothing fancy. The problem is getting something in orbit or returning something back to Earth in one piece. Cheaply.
It seems that most voters at XPrize believe that the SCALED COMPOSITES, LLC have a better chance to take home the XPrize than Armadillo Aerospace.
With shock absorbing crash couches and a reclined position, higher vales should be possible. The issue is failed parachute depolyment. Single parachutes may deploy incorrectly or not at all increasing the G load. Normally a cluster of parachutes are used hence the margin needed for error. Without access to the web site, I can't see how many chutes were being used.
See my journal, I write things there