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Our seafaring nature hastranslated well to the space age,
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sailing out into the unknown insearch of riches of one kind or another.
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While Europe and Asia continuetheir interest in the resource-rich Moon,
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the United States and NASA have settheir sights on nothing less
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than manned missions to Mars.
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Can they manage to go shore to shore
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on the most dangerousof unknown seas, deep space?
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With low Earth orbit harnessed,it is time to look further afield.
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To build a spacecraft and rocketsystem to reach Mars
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is a mammoth undertaking,
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but if successful,it will return the United Statesto the topof the space achievement ladder.
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The first requirement:
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a space capsule able to carry sixastronauts for a long period of time
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and return them safely to Earth.
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Orion is its name and it has flownonce already in a shakedown.
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The next flight will bean unmanned test mission past the moon,
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followed by a third manned mission.
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The components for the vehicle aredeveloped around the country,
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tested and checked,then passed on for assembly.
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The minutest bolt and circuit isdesigned, tested, redesigned
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and tested again.
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Slowly the systems come together,
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with the aid of somebreakthrough technology,
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particularly in manufacturing methods,new materials and processes.
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The first thing to notice isthat NASA have gone back
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to the classic conic shape like Apollo,the safest design yet devised.
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Avionics, control systems,computer software and a glass cockpit,
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all state of the art.
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...and the concept was to go
with a glass cockpit
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and what that means is
that the instruments are all images
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on a computer screen.
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They are all on glass,
so rather than flipping a physical switch,
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the crew brings up a computer screen
and flips a virtual switch,
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a little icon of a switch
or icon of a valve,
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and with the exception of seven panels
right around the computer screens,
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which have about 60 switches,
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that is all of the cockpit of Orion
happens on the glass.
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One big benefit is the weight savings
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because you don't have to have
a physical switch.
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And having a physical switch,
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not only
is there the weight of the switch,
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but you also have the weight of the wire
to the switch,
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and you have to have the weight
of circuitry that takes that wire
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and feeds it into the vehicle computers.
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Because of Orion's size,its all-important heat shield
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is the largest one ever made,
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and new processes were requiredto manufacture it.
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The Orion heat shield has
got to be able to withstand landing loads
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on the order of 300
to 400 thousand pounds.
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Because we're returning potentially
from the Moon or beyond
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and the flight duration from the time
in which you commit to a return
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to the time you actually land,
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the weather conditions on Earth
can be substantially different
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or difficult to predict.
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And so the Orion spacecraft has to be able
to land in the ocean
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in a wide range of sea conditions,
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wave height, wave slope angle
and horizontal winds.
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That is what's driven us to a skin
stringer architecture that utilizes
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a thick laminate composite skin
bolted to a titanium sub-structure.
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We bond on an ablator, called the Avcoat.
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The ablator is the thermal protection part
of the heat shield.
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The very outside of the ablator
actually gets hot enough
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that it decomposes,
and that's the ablation part of it,
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as opposed to an insulator
like a shuttle tile.
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Then come the ancillarystructures and equipment
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that will ride with the capsule.
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The escape tower, designed and tested,
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will pull the capsule awayfrom the main rocket
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in the case of an emergency.
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Adaptor separationfrom the rocket's upper stage.
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Parachute deployment.
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The connecting adaptor to the EMS.
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The EMS is the service moduleattached to the Orion in flight,
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supplying oxygen,water, power and heating.
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Built by ESA, it is basedon their very successful ATV program
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which delivered supplies to the ISS.
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It'll also provide the main engine thrustfor deep space maneuvering.
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We have, in particular,
a very, very tight schedule in front of us
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so everybody's working under high pressure
to meet the dates
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and this requires
a very, very close collaboration.
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I see a very motivated team,and so far, as an agency,
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we are quite happy with the performanceof the European industry.
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The US Navy is tasked withretrieving the capsule from the ocean.
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At first they train in the pool,then calm waters,
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then the Pacific,and finally the real thing.
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Experts continue to evolvethe process and training
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in readiness for the day whena manned flight returns from deep space.
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This is the RS-25,the Ferrari of liquid rocket engines
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and the main enginefrom the Space Shuttle program.
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Economically re-purposedfor the Space Launch System,
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four of these engineswill power the main stage of the rocket.
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The main solid rocket boostersof the shuttle program
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also have a renewed lifein the SLS.
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With another two segments added,
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the boosters will thrustfor over two minutes.
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This project has been
a real fun effort in trying to take a heritage booster
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that had many, many years
of reliability and great performance and evolve it
into something bigger and better.
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When we first undertook this design
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and qualification
for the new booster,
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part of the mission
was to make the booster
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more affordable and more modern
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and, of course, it had to be completely
redesigned for a new mission.
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It's a larger booster
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and the mission profile
is sufficiently different
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to where pretty much everything
on the inside of the booster is different.
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There's well over a thousand
individual processes.
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Working with our customer,
we were able to identify
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several hundred areas of improvement.
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We've got totally new avionics
on this vehicle
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versus what we had on Shuttle.
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It's state of the art.
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Bigger and more powerfulthan any previous launch system,
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the SLS has been under developmentfor some time.
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Designing it is one thing,building it another.
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In new or refurbished factoriesand assembly shops,
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the body of the largest rocket ever to flyis being constructed one piece at a time.
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The massive hydrogen tank takes shape.
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The smaller oxygen tank soon follows.
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The interim stage for the mannedflight is another hydrogen-oxygen motor
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supplied by cryo tanksfabricated with new technologies.
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So to design and manufacture
this tank, we used new materials.
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We processed the tank
by automatic fiber placement.
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The benefit of that is
we can lay down the material quickly,
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which provides us a low cost operation
and a very lightweight tank.
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Well, we've worked on this program
for 29 months and when we started,
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we'd never built a tank of this size
by the methods that we did.
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We did automated fiber placement
and fluted core,
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just developing the robotic
fiber placement equipment
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in a way to make the skirt in one piece
was a large challenge.
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Each exacting pieceis fabricated,
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test articles are runthrough the mill,
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vibration tests, vacuum tests,acoustic tests, stress tests.
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Nothing is left to chance.
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New technology and new materialsfor a new generation of space exploration.
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For this test, there wereseveral things that we looked at.
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This was the first time we usedthose thermal knives
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to start the deployment sequence.
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And that allowed cuts and tethers,
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but then allowed the solar arrayto deploy.
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We wanted to test the locking mechanismsto ensure that it locked properly in space
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because anything that could possibly gowrong, we wanted to see tested down here,
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so we can ensure, you know,a successful flight.
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It's all about technology.
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If you don't develop technologies
for the future,
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you won't go where you want to go.
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So composites will decrease
the weight of the tanks.
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It'll increase the payload performance
of the launch vehicle.
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It'll give us-- it basically enables
things that we don't have today.
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Soon the mighty rocketwill lift human beings up further
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than ever before.
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The flight to Mars will be a long one,too long for a crew to sit in a capsule.
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A habitat and supplies will alsobe lifted to orbit and assembled.
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Several companies have been selectedby NASA to carry out studies
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for a suitable system to do the job.
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A bit of competitionis always good for invention.
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Bigelow Aerospace with itsExpandable Activity Module, or BEAM,
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currently being tested on the ISS,
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will develop and test a prototypeof XBASE,
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a 330 cubic meter expandable habitat.
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Boeing of Houston is developinga modular habitat system
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that leverages more than 15 yearsexperience in designing, developing,
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assembling on-orbit,
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and safely operatingthe International Space Station.
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Lockheed Martin will refurbisha multi-purpose logistics module
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into a full-scale habitat prototypethat will include integrated avionics
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and ECLSS.
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Orbital ATK will maturethe mission architecture and design
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of their initial cislunar habitat concept,
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based on the Cygnus spacecraftthat now supplies the ISS.
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Sierra Nevada Corporation'sSpace Systems will study and refine
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a flexible architecture and conceptof operations
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for a deep space habitatthat draws on the lessons
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of three to four commercial launches toconstruct a modular long-duration habitat.
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NanoRacksin conjunction with its partners,
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Space Systems Loraland the United Launch Alliance,
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referred to collectivelyas the Ixion Team,
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will conduct a comprehensivefeasibility study
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regarding the conversion of an existinglaunch vehicle's upper stage,
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or propellant segment,
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into a pressurized habitable volumein space.
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So if you're designing
spacecraft to be in the Mars orbit,
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then the studies we're doing
on Space Station can be applied
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and help us to design more durable
spacecraft for that Martian atmosphere.
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MISSE stands for the Materials
International Space Station Experiment.
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We do study the durability of polymers
in terms of their mechanical properties
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with radiation exposure.
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And we hear a lot about the radiation
exposure impact on humans
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for flights to, say, Mars,
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but polymers and other materials
that are used on spacecraft
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can also degrade from radiation
and that's one of the things I study.
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The MISSE experiments do take
a bit of time because we do very careful
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dehydration measurements of
the samples after they've been in space.
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What we've found is
that the Teflon erosion rate
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is highly dependent
on the amount of sunlight
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and possibly the heating too.
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You need to know which of these
environments it's gonna be exposed to
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because it'll erode at a different rate,
depending on the environment.
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Assembling spacecraftin orbit
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and fueling them for the long journeyto Mars sounds simple enough.
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On orbit,refueling is anything but simple.
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NASA have been developing a system forunmanned refueling for quite some time,
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and have a test article onboard the ISS.
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We can take
a pick-and-place robot,
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put the tool
wherever we need it to be,
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and all it needs to do is drive that tool
because the smarts are in the tool.
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So, that's what we learned
from working on Hubble is
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you put a smart tool
with the astronauts
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and accomplish, you know, both things.
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You've got smart tools
and astronauts working together.
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Now we're putting smart tools with robots
and trying to accomplish
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the same type of things we did on Hubble.
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Aimed at developingcapabilities for servicing,
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even refueling spacecraft on orbit,
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RRM is likedoing precise surgery at a distance,
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doctor and patient separated by the voidand vacuum of space.
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It's tough, but the payoff is huge.
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Robotics can do things
that humans can't do
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in terms of precision,
in terms of control.
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Holding a particular spot for six hours
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while engineers on the ground
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debate what to do.
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We can't ask a human to do that.
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The robot is a very stiff,
rigid interface.
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It's not forgiving,
like an astronaut's hand,
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so we have to take that into account.
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When you push on something really hard
with the robot,
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you build up really large
contact forces.
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When the astronaut pushes on something,
his wrist might give--
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you know, he's got his own
internal software compliance running.
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But in order to accommodate the robot
so we don't break anything,
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we have to build features into the tool,
features into the software,
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just getting the robot
to go where you want it to go.
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You know, they don't position precisely,
so you have to do things like
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build lead-in into the tool.
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An astronaut can probably just get it
right on there because he's right there.
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So we do have to do things to make them,
you know,
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very specific to robotic operation.
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We're almost there.
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Whoa!
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That task successful,next stop Mars.
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The first manned mission to Marswill probably only orbit the planet,
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checking out all the gear and processes,
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even launching communicationsatellites and finalizing landing sites
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in preparation for the next mission,
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which will then make the descentto the surface.
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And that has a whole newset of problems to overcome.
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Unlike the moon,Mars has stronger gravity,
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about knot .6 of Earth's,
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but it does have an atmospherewhere parachutes can be used,
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although the atmosphere is very thinand not very deep.
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Well, it's a funny thing about Mars,
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but if you take the average
of the planet,
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the average height of everything
in the planet,
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it turns out that most of
the north is two kilometers below that
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and most of the south
is two kilometers above that.
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And it's just, we always land in the north
'cause there's a lot more atmosphere.
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If you land in the south,
it's like four kilometers less of air
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to come to a stop.
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In fact, at the altitude of the mountains
in the south,
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the Mars science laboratory
was still supersonic
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as it was descending into the crater
it was reaching in the north.
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Assuming the need topre-position habitats, supplies
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and equipment on the surfaceprior to humans landing,
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NASA and its partnersare looking at several solutions.
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One is the HIAD or HypersonicInflatable Aerodynamic Decelerator.
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This is basically a very largeinflatable heat shield,
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much larger in areathan the payload,
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able to slow the craftconsiderably fasterthan a standard spacecraft heat shield.
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Plans are to test the systemon a payload from the ISS,
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utilizing a Cygnus resupply spacecraft.
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Once lower in the atmosphere,parachutes will further slow the payload
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to an altitude low enoughfor rocket engines to take over.
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Morpheus and the Xombie flightsystems have matured
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over the last few yearsand are capable of delivering cargo
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to a planet's surface autonomously,
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avoiding rough terrain or other obstacleswithout human intervention...
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...adding yet another building blockto our human effort
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to explore the solar system.
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