t/Space Demonstrates New Air-Launch Method
FleaPlus writes "Last month t/Space, an organization with plans for constructing a simple, low-cost successor to the Space Shuttle, was mentioned on Slashdot. Recently t/Space used a portion of the concept study funds it had been awarded by NASA to also build and test actual hardware. They performed three weeks of drop tests of a 23%-scale model from a Scaled Composites Proteus carrier aircraft to demonstrate the feasibility of a new air launch method they had devised, dubbed 'Trapeze-Lanyard Air Drop.' The new method eliminates the need for wings on air-launched rockets, potentially leading to improved safety and cost-effectiveness. Last month at a space conference they also displayed a full-scale model of their vehicle. Unfortunately, with the recent selection of Boeing/Northrop-Grumman and Lockheed-Martin as the two competing teams for the contract to build the Shuttle's successor, t/Space's future path is somewhat uncertain."
..dubbed 'Trapeze-Lanyard Air Drop.'
..I'm pretty sure I saw this on Jackass..
Starsucks
If we could just get rid of combustion and the need for incredibly expensive fuels... we'd be set.
u nd/facts/vcd.html
Elecromagnetism? Superheated water / water reclamation?
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http://www.nasa.gov/centers/marshall/news/backgro
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t/Space's future path is somewhat uncertain."
Given the possible boom in space tourism, I dont see t/Space going out of business anytime, especially if they have a viable technology.
If NASA will not fund it , they can find private investors and start the private space industry ...
Damn it, Beautrice... that's something different :)
http://www.eng.titech.ac.jp/jyosei/t_yabe.pdf
That is more along the lines of what I meant!
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Although Boeing-Northrop-Lockheed are the big boys right now, I dont see why one of thsoe teams wouldnt be capable of choosing t/space for crew-space transfer =) Then again Boeing-Northrop probablly wouldnt since Northrop is only involved in spiral 1, but Lockheed might.
Also, Griffin has made it quite clear that he wouldnt probablly fund t/space, BUT if they do get a vehicle built and it is cheap, he will gladly use it for crew and cargo transfers to the ISS.
Was it just me, or did anyone else read that as a Scaled Composites Protoss Carrier aircraft? I guess we better start building our Science Vessels!
This gradual progression of space technology is ok, but we really need to step it up a notch. And we all know the coolest tech is made during times of war. So how about it? How can we start this space war we so desperately need? Hell I will have no problem joining the army if I get a space fighter.
Missile technology is basically a guided, long range bullet.
Job? I don't have time to get a job! Who will sit around and bitch about being broke and unemployed then?
i wonder how many days (weeks?) are spent on training astronauts to use this throne?
and now back to the fallout shelter...
Whatever happened to launching from lighter-than-air platforms? With conventional rockets, so much weight goes into fuel to move the fuel you'll burn later to move the fuel that comes even later. Surely someone's doing something with a straightforward idea like this?
If I read the article correctly, tspace and scaled composites are after the crew transport vehicle portion of the new nasa vision. That is, the capsule to get to the crew exploration vehicle or the iss space station. The sole purpose of the ctv is to get people in low earth orbit from an in atmosphere launch using a pre-existing capsule design.
I think the contracts for cev were awarded to northrop/grumman and boeing for a 2 party competition. That is, the crew exploration vehicle which resides in space.
Though, nasa might fund them $400m for a alternate/creative role in the process. Who knows, now wouldn't be funny if they could pull it off with the limited funding? That would prod the bigger companies which would be good.
The beauty is if they can get rid of shuttle the savings will pay to get to the moon. The moon has its own resources which could be used to create launches/refueling from the moon and not earth.
http://www.hobbyspace.com/NearSpace/index.html#Roc koons
I think you're thinking of these. They do work, it's just that you have to deal with the time and danger involved with a baloon ride before firing the rocket, while going up in a powered aircraft like a plane gives you more control.
A blimp like thing (lighter than air, powered and with a lifting body profile) that might be nice. That's a whole nother aerospace engineering project in itself.
The overwhelming majority of fuel used to launch spacecraft is spent accelerating the rest of the fuel. If you don't carry the fuel with you, it will take much less energy to reach orbit. Consider the European Union's Hopper which will accelerate spacecraft on magnetic rails. They already have a prototype.
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eh eh they think they have everything
All t/Space needs is to get a couple dozen congressmen in its pocket and boom! ...in like Flint.
Let's face it...the manned space program is a slush fund for well-connected defense contractors.
P.S. Did I mention the "word in image" thing still sucks donkey balls?
Just because space travel is costly for NASA doesn't mean it must be for the rest of us. As soon as it's profitable to do without NASA level budgeting, companies will scoop up the benjamins like there's no tomorrow.
The question is: was that 23% the size or 23% scale model, because those are two vastly different volumes.
And the corollary question is: was it an empty shell? or did it have the same mass distribution that the rocket will have?
Can you be Even More Awesome?!
agreed.
That's baloney. The US military loves the air launch thing. Back in the '70s there was a pathfinder-type mission that air launched a Minuteman. And the MDA is heavily invested in air launched targets for the various interceptor programs. There was the LRALT program and a newer target launched by Orbital Sciences. And, of course, there's also Orbital's Pegasus space launch vehicle.
The benefit of the type of air launch method that t/Space is showing is that the LRALT and MRT programs require the extremely heavy sleds that they sit on and that they are limited by the cargo capacity of a C-17. And Pegasus has to carry that enormous wing and tail structure (not to mention its failures, such as the first X-43A flight).
I think if t/Space can show superiority over the existing air launch methods (which doesn't seem to be difficult), they will definitely fill a demand in both the small space launch and targets markets.
Not sure if this is routine but apparently it's been done on a larger scale
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http://www.spaceref.com/news/viewpr.html?pid=1661
wonder how hi proteus was when it dropped the capsule
If nobody fucked the space between our mothers' legs, none of us would be here.
That trapeze system looks like something used in the 50s and 60s for large missle launches off USAF jets. I think the Genie used a trapeze to launch from an F104.
wow, you're intelligent. That is what it boils down to with the anti-space, anti-progress, anti-tech crowd. Fuck space, right? Go live in a cave, AC. You are in the "get out of the way" part of LEAD, FOLLOW OR GET OUT OF THE WAY!
OMG! It's 2am and I fell for a troll.
gigantino.tv - Heavy but weighs nothing.
now if they could only design some 23% scale modeled astronauts t/Space would be in business.
Gary Hudson, the chief scientist at t/Space, has been trying to spark the spaceflight revolution for 30 years. He had a rocket called Conestoga in the 80s that ran into the infamous "brother-in-law problem" at NASA. He was also the driving force behind another Mojave airport first: the Roton demonstrator. Now he's back with the world's most famous aircraft designer and a bunch of other people from the space activist community.
Burt needs no introduction: he's da man. Burt builds the coolest planes in the world and has finally started building spaceships.
So, t/space has been doing droptests, excellent! They have a great capsule demo and seem to be trying to stretch their funding as far as possible. I'm pretty sure they said that the "CXV" was proposed specifically outside the CEV RFP, because they refuse to fill out that much extra paperwork. You can see what Mr. Hudson was working on in the early 00's here: http://hmx.com/ The pdf is his proposal for a capsule (manned/cargo) for the old Alternative Access to Station program, gives a good idea of where the CXV's heritage is.
t/space is an amazing team. If they can keep the funding coming, they will deliver on this craft.
Josh
gigantino.tv - Heavy but weighs nothing.
is MORE safe? Personally I like my aircraft to have wings thankyouverymuch.
the tether held on to the package until after the motors had achieved sufficient thrust and then released it... that way, if the engines don't make it, they can be shut down and the very expensive package retrieved by means of a winch... if needs be, jettison the motor bit and just retrieve the payload.
Donald 'Duck' Dunn: We had a band powerful enough to turn goat piss into gasoline.
we could have this "rocket" thats being dropped have a canon on it that shoots astronauts into space from a high altitude.
If at all plausible from a technical standpont, space elevators are probably the most sensible way for sending humans or loads to space. If you can't beat gravity, use it. Armchair engineers can send in their entries.
I'm a sci-fi vegan: I don't want the aliens to think we have as much right to live as the fried chickens we eat.
You can air launch a pretty good sized vehical. A 747-400F can lift over 120,000kg A mission specific aircraft could probably do much better.
I don't know about manned but for sats it may be the way to go.
See my blog http://ilovecookes.blogspot.com/ for light hearted technical information.
Unfortunately, with the recent selection of Boeing/Northrop-Grumman and Lockheed-Martin as the two competing teams for the contract to build the Shuttle's successor, t/Space's future path is somewhat uncertain.
I would think their path is clear: Get one of those other two to buy them!
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If only we could figure out how to build a safe nuclear launch vehicle. The energy density of nuclear fuel is something like a thousand times larger than that of chemical fuel.
Maybe you could put a reactor into an upper stage and heat something like water in a closed cycle for launch. Steam would power turbofans for vertical or horizontal liftoff. At say 50,000+ feet or so, the first stage with turbofans separates exposing nozzles for the fluid to be ejected as rocket exhaust. Now the reactor cranks up the heat higher on the working fluid and uses it directly as propellant.
I don't know. Are there any actual good designs for nuclear launch out there? I saw something about RITA, but it didn't have many details.
I'm sure you are already familiar with the work of Leik Myrabo , but in case you aren't, you ought to check out his stuff. He is the big pioneer in this area (ref. 3 on your correct link).
You are right that huge savings can be had by separating the power source from the vehicle - Myrabo was writing about this 20 years ago. Most of the energy used by a rocket is used to elevate the fuel to the altitude at which it is burned. If the energy is supplied to energize a propellant (such as vaporized water as suggested in your link), the amount of propellant can be much less than the amount of burning fuel would be. Unfortunately, Myrabo has focused his more recent efforts on rather weak air propelled engines which haven't had much punch.
Because the real limit in terms of how much propellant is needed depends upon the specific energy (and thus the temperature) to which the propellant is energized, it is best if the propellant is heated to a very high temperature. For these purposes, an concentrated ultraviolet light source would work as well as a laser, and would likely be much cheaper than a fairly efficient laser of high power. Also, if a laser is used, the best case scenario would be if the photon energy corresponded to a particular energy jump in the target propellant, similar to the way an excimer laser is used. In the case of simply heating the propellant, material considerations will limit the amount you can heat the material (i.e. at some point, your water vapor will melt the nozzle). However, in the case of the excimer laser, a solid propellant could be used which would not suffer from heat transfer from the solid/gas interface, which means really high specific energies could be used.
Which means you can put 5-10,0000 kg in LEO, depending upon how good your rocket guys are. Which is decent. But chances are you are going to have to structurally reinforce that 747-400F to carry the rocket, which will reduce the weight, etc... its a system of trades. But even still no reason it couldn't be used as a launch platform for an ISS ferry vehicle.
The downside is, now you are launching from a moving platform. And the savings, while there are some, arent **that** great... IE, you aren't going to be able to pull off a single stage rocket unless you have some amazing rocket guys working for you and you are putting a very minuscule package in orbit. 2 stages from the earth's surface is easy enough, if you are adding the complexity of an air launch you would want to get some benefit of complexity reduction out of it (And staging is a good source of failure...)
-everphilski-
> t/Space's future path is somewhat uncertain
If the idea is that good, one or both of the contractors could license it from them. Could be very profitable for t/Space. Also likely: they get bought up by one of the big guys.
t/Space recently released a paper with more details of the air-launch method and the flight tests here:
t LAD_Test_Program.pdf
http://transformspace.com/document_library/media/
Should be able to put it into a relatively gentle parabola and simply kick your 56.7t load out the tail.
Small disposable drogue goes first to make sure payload points the right way throughout (would be the world's most expensive air-air missile if it destabilised and happened to point the wrong way when it went whoosh), slide out back end, (roll and?) send C5A into negative gees to miss the payload, light blue touch-paper, home time.
Got time? Spend some of it coding or testing
...'tis supposedly able to do 110t over shorter distances - but I don't think it says anywhere "in one lump". (-:
Got time? Spend some of it coding or testing