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(futuristic dramatic music)

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(rocket engines sizzling)

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NASA certainly was the shiny light,

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the benchmark of American aspirations in the '60s.

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The large Saturn V rocket, the Lunar Rover,

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the little moon buggy,

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all of that was something that I wanted to do

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when I got older.

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I wanted to put people on the moon.

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I wanted to put people on Mars.

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We leave as we came,

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and God willing as we shall return.

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I joined NASA in 1976 during the early development

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of the Space Shuttle Program.

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Preflare maneuvering

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will pull the nose up a little bit,

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right before it hits the runway.

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The Space Shuttle became that goal of low-costs

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to low Earth orbit.

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I always felt like it was an interim period

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in our history.

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(rocket engines blasting)

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To me, NASA's role was always to go deep into space.

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Thank you.
(audience clapping)

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A little more than 40 years ago,

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astronauts descended the nine rung ladder

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of the lunar module called LEM.

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When President Obama made the announcement in 2010

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that NASA's role is deep space.

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The question for us now

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is whether that was the beginning of something

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or the end of something?

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We were all excited.

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I choose to believe it was only the beginning.

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It's definitely a Kennedy moment

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when you can say, "We're gonna do

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"something that's never been done before,

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"not only go to the moon, but onto Mars."

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I was in high school when Barack Obama made the speech.

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So for me, I looked at it as an opportunity

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to be able to have my footprint

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in human exploration history.

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Permanent presence on the moon,

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people have dreamed of this for years.

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The Obama decision kind of lit a little fire

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that has gotten bigger.

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Going back to the moon and going to Mars,

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that's my generation of engineers who are gonna be

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the pioneers to send humans to Mars.

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(dramatic music)

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For some of us that have only known low Earth orbit,

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it was a daunting idea.

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It told us that we were gonna need

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a tremendously large rocket.

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(dramatic music)

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The magnitude, both in power and in size.

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Not just heavy lift, but super heavy lift.

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(rocket engines blasting)

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It's NASA, most powerful rocket ever,

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a machine built to allow humanity

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to explore the moon and beyond.

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(upbeat music)

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This is the story of the mighty Space Launch System, or SLS.

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(dramatic music)

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With a Space Launch System, the stars are our destination.

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(dramatic music)

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But we haven't developed anything like SLS

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in, literally, 40 years.

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(dramatic music)
(rocket engines blasting)

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And so we're having to start from scratch on,

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"Hey, how do we get to the moon?

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"What do we need?"

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(dramatic music)
(rocket engines blasting)

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The questions that arise are,

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who has the expertise even to do the same thing,

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but also to do it better or differently?

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(dramatic music)

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(pondering music)

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July, 2013,

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NASA has preliminary plans for the Space Launch System,

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a rocket designed initially to take astronauts

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back to the moon on a mission

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that will come to be called Artemis.

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Engineers need to create a machine that surpasses

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the legendary Saturn V,

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the rocket that launched the Apollo moon missions.

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But no one has built a rocket that powerful

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in over 40 years.

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(pondering music)

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We had nobody that had hands-on experience

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of a rocket like that.

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But we had a young cadre of engineers

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who really wanted to get their hands dirty.

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We really didn't have a lot of hands-on experience

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in working with these large scale engines.

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So one of the ideas they had was to take apart

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a Saturn V first stage engine.

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This new F1 must perform perfectly,

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for more than just time and money are involved:

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men's lives will depend on it.

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Why don't we go get one of the F1 engines

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out of the Smithsonian and a tear it down

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and reverse engineer it.

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We just said, "Hey, let's get a big crane

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"and let's pick it up and go put it

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"into a big building and let's start taking it apart

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"and seeing what made it tick?"

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(pondering music)

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It did have a few pieces of bubblegum

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from being in the museum and some kids walking by

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and sticking some bubblegum on the side of it,

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but it was still in really good shape.

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(pondering music)

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When we started to dig into it and take it apart

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there was still kerosine, there was still rocket fuel

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left in it from when it was tested back in the '60s.

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So to touch it, to smell it,

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to get the soot that was still on the turbine blades,

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it was just a, it just hit every sense in your body.

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The pride that someone had put into making these complicated

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and difficult welds, and they were all done by hand.

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To me as an engineer,

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if you wanna look at how well something's made

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you go look the welds,

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and every one of those on those rockets is flawless.

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(pondering music)

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What we ended up with, really,

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is a team of hands-on engineers that were young

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and not ready to retire,

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and they wanted to go actually do this.

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Saturn V may have been the inspiration,

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but for most of the SLS design,

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NASA turns to a more recent launch system.

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The Space Launch System is a combination of new and old,

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and actually quite a bit of old.

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And the Shuttle has cleared the tower.

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Legacy parts inherited were not just

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from the Apollo program,

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but actually from the Shuttle era,

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which, I think, is maybe more relevant.

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(rocket engines blasting)

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Saturn V is the grandparent of SLS

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and Space Shuttle is the parent.

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SLS will use modified

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Space Shuttle main engines and enlarge versions

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of it's Solid Rocket Boosters, pushing them to the limit,

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using modern digital technology.

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We have taken the Space Shuttle,

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we've taken the orbiter off of the side of it,

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we've put the orbiter's engines under the bottom

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of the vehicle.

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We've lengthened the Solid Rocket Booster,

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and we've stretched the tank to get more fuel on board.

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(dramatic music)

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It sounds really simple,

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(dramatic music)

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but there was much more complexity to doing that

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than first meets the eye.

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(dramatic music)

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With a new team in place

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engineering for SLS is underway,

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(engines firing)

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and the first step is an essential data gathering mission.

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How do we use parts that were intended for one purpose

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and apply them in a different environment?

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Air dynamics is a huge part of building any launch vehicle.

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We do test models in wind tunnels

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up to around 13-feet long.

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(light dramatic music)

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(dramatic music)

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One of the key areas we test first is this area of flow

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that we call transonic, and shockwave start to occur.

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This compression of air molecules at different parts

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of the rocket.

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(dramatic music)

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One of the complexities of SLS is due to its extreme size,

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the larger the structure, the lower its natural frequencies.

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(dramatic music)

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When you go through the transonic region,

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shocks are trying to form on the side of the vehicle.

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(upbeat music)

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Then you have to worry about coupling up that dynamic

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with the natural frequency of the vehicle.

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And when I say coupling,

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I mean that the frequency at which I'm pulsing it,

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is also the frequency that the structure wants to respond,

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and so they're having a good time with each other.

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In the engineering world, positive reinforcement

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is usually bad.

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(rocket engines blasting)

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Those kinds of dynamics you can literally break things,

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you can cause pulses that even influence

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the thrust of the rocket engine.

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Using a combination of aerodynamic

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and acoustic testing engineers reach a troubling conclusion.

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Early on we realized that these parts

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that we inherited from the Legacy Shuttle Program

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really were not capable of flying through transonic.

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(dramatic music)

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Rocket components are not universal.

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They're all designed and optimized

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for the vehicle that they are built for.

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Space Launch System has four engines,

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the Shuttle only had three engines.

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Space Shuttle had them

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on the back of the actual plane itself.

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For Space Launch System,

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we put them at the bottom of the borough.

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(dramatic music)

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So on Space Launch System now,

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those components are gonna experience

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much more violent vibrations.

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So the size requires, as a propulsion engineer,

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requires us to make sure that those parts

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can withstand the new vibration, the new loads.

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We took those original components from the Space Shuttle,

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and we had to make them thicker and beefier

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to deal with the weight and the structural movements

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and the size of the Space Launch System.

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(dramatic music)

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(pondering music)

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Beginning in 2013,

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the Michoud Assembly Facility in New Orleans,

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a vital part of the Space Shuttle Program

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must be extensively refitted to cope with the size of SLS.

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But by November, 2014,

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the first pieces of the SLS core stage

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are coming out of the factory.

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(upbeat music)

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The 8.4 meter diameter is exactly the diameter

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of the external tank on Space Shuttle,

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but we've stretched the tank to get more fuel on board.

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The core stage diameter is the same as what we flew

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on Shuttle, but that was really not driven

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as much by vehicle architecture

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as by taking advantage of existing tooling

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and infrastructure capabilities.

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If I can use the same machines,

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I don't have to buy new ones.

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The core stage is the biggest stage

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that we've ever built, and in fact,

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the hydrogen tank is the biggest tank

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we've ever built.

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Each tank is made in sections,

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joined together by a technique called friction stir welding,

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a spinning tool heats up the metal of the two edges

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until they become soft and stirs them together

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like mixing dough.

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The resultant joint is strong and light,

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but refining the process to ensure defect-free welds

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was a challenge.

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We pushed the technology of friction stir welding

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with this tank.

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I don't think anybody's ever seen anything like it before.

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(light upbeat music)

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With SLS, NASA is pushing at the limits

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of what is possible because there's a fundamental reality

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that governs all rockets.

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(rocket engines blasting)

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You have this thing called gravity,

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yet, we have to overcome that and go beyond.

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Behind every aspect of the SLS design

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is a single mathematical formula.

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In order to understand how a rocket actually works

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we have the the rocket equation.

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Oh, to me, the rocket equation,

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you know, you might as well just tattoo that on my arm.

268
00:13:09,790 --> 00:13:11,590
It's what makes makes all this work.

269
00:13:12,535 --> 00:13:17,535
(rocket engines blasting)
(dramatic music)

270
00:13:18,560 --> 00:13:21,330
You're looking at the incremental effects

271
00:13:21,330 --> 00:13:24,990
of how you're releasing mass in order to achieve

272
00:13:24,990 --> 00:13:26,283
an escape velocity.

273
00:13:28,620 --> 00:13:31,050
You know, it's Newton's law: reaction and reaction,

274
00:13:31,050 --> 00:13:33,240
you're throwing out at fast speeds

275
00:13:33,240 --> 00:13:34,993
a lot of dense propellant.

276
00:13:36,960 --> 00:13:38,790
You wanna take your mass and you accelerate it,

277
00:13:38,790 --> 00:13:40,290
then it produces force, right.

278
00:13:43,150 --> 00:13:46,360
The real crux of the matter of the rocket equation

279
00:13:46,360 --> 00:13:50,643
is I want most of the weight of my vehicle to be propellant.

280
00:13:53,630 --> 00:13:56,010
It puts you in a little bit of a box

281
00:13:56,010 --> 00:13:59,440
because I'm trying to get more and more fuel on board

282
00:13:59,440 --> 00:14:02,063
that my tanks are getting bigger and bigger.

283
00:14:03,450 --> 00:14:06,563
Now I'm fighting the weight of the structure itself.

284
00:14:07,590 --> 00:14:12,000
Every ounce of weight that I change greatly impacts

285
00:14:12,000 --> 00:14:13,883
the bottom line of the rocket.

286
00:14:15,370 --> 00:14:17,800
There is a risk you'd have a vehicle that's too heavy

287
00:14:17,800 --> 00:14:19,460
and might not have enough propellant.

288
00:14:19,460 --> 00:14:21,420
And the rocket equation would get you again,

289
00:14:21,420 --> 00:14:23,920
and you'd run out of steam before you got to orbit

290
00:14:26,700 --> 00:14:27,830
The rocket equation, you know,

291
00:14:27,830 --> 00:14:30,500
the part that we focus on is the part we can control, right,

292
00:14:30,500 --> 00:14:31,750
it's a physics-based equation,

293
00:14:31,750 --> 00:14:34,970
and so we can control the fuel economy

294
00:14:36,610 --> 00:14:39,320
and how do we optimize the mass?

295
00:14:39,320 --> 00:14:40,650
I don't wanna say minimize the mass,

296
00:14:40,650 --> 00:14:45,290
I wanna say optimize the mass because it takes mass

297
00:14:45,290 --> 00:14:47,930
to build a structure that can handle the loads

298
00:14:47,930 --> 00:14:49,554
that we put it through.

299
00:14:49,554 --> 00:14:52,770
(pondering music)

300
00:14:52,770 --> 00:14:55,853
And there is a limit to how big you can make something.

301
00:14:57,053 --> 00:14:59,886
(pondering music)

302
00:15:01,650 --> 00:15:05,350
In April, 2017, the first completed section

303
00:15:05,350 --> 00:15:10,150
of the core stage begins a 1,240 mile journey,

304
00:15:10,150 --> 00:15:12,143
from New Orleans to Alabama.

305
00:15:14,970 --> 00:15:17,700
The engine section test article will be carried on

306
00:15:17,700 --> 00:15:21,313
NASA's Pegasus barge to the Marshall Space Flight Center.

307
00:15:23,500 --> 00:15:26,370
There, it will undergo structural tests

308
00:15:26,370 --> 00:15:28,620
to ensure it can withstand the forces

309
00:15:28,620 --> 00:15:32,283
created by 8.8 million pounds of thrust at launch.

310
00:15:34,161 --> 00:15:36,980
(dramatic music)

311
00:15:36,980 --> 00:15:39,710
Many, many different components of the Space Launch System

312
00:15:39,710 --> 00:15:41,610
lie within that one engine section.

313
00:15:41,610 --> 00:15:44,080
I would even say about 80% of the parts

314
00:15:44,080 --> 00:15:47,573
that go into the core stage is in the engine section.

315
00:15:48,603 --> 00:15:50,340
(dramatic music)

316
00:15:50,340 --> 00:15:53,370
It's one of the most important segments of the core stage

317
00:15:53,370 --> 00:15:55,070
for the Space Launch System,

318
00:15:55,070 --> 00:15:58,843
because it attaches the RS-25 engines.

319
00:15:58,843 --> 00:16:01,676
(dramatic music)

320
00:16:05,420 --> 00:16:07,870
16 Shuttle main engines were leftover

321
00:16:07,870 --> 00:16:12,870
after the Shuttle program ended in 2011 called RS-25s.

322
00:16:13,510 --> 00:16:15,563
They already have a proven track record.

323
00:16:16,670 --> 00:16:18,360
(pondering music)

324
00:16:18,360 --> 00:16:20,940
The RC-25 engine, it's a seasoned veteran,

325
00:16:20,940 --> 00:16:23,450
it's been aging well like wine, right,

326
00:16:23,450 --> 00:16:24,760
it gets better as we age it

327
00:16:24,760 --> 00:16:26,449
'cause we implement improvements.

328
00:16:26,449 --> 00:16:29,760
(pondering music)

329
00:16:29,760 --> 00:16:33,430
For a car guy I would say they are the Rolls Royces

330
00:16:33,430 --> 00:16:36,593
and the Ferrari together as an engine.

331
00:16:37,620 --> 00:16:39,440
I have to put this in there as well.

332
00:16:39,440 --> 00:16:42,111
They also have a little Prius built in there. (laughs)

333
00:16:42,111 --> 00:16:44,000
(light dramatic music)

334
00:16:44,000 --> 00:16:48,300
In 2014 NASA begins shipping all 16 engines

335
00:16:48,300 --> 00:16:50,990
to Stennis Space Center where they must be refitted

336
00:16:50,990 --> 00:16:52,503
for Space Launch System.

337
00:16:53,880 --> 00:16:57,210
We needed to adapt those engines, it's a different rocket.

338
00:16:57,210 --> 00:16:59,930
There were interfaces that had to be dealt with,

339
00:16:59,930 --> 00:17:03,960
physical, mechanical interfaces, hydraulics, gases,

340
00:17:03,960 --> 00:17:06,723
propellant, a lot of things to think about.

341
00:17:08,320 --> 00:17:10,450
The engines burn liquid hydrogen

342
00:17:10,450 --> 00:17:14,160
and oxygen to create superheated water that exits the nozzle

343
00:17:14,160 --> 00:17:18,083
at 13 times the speed of sound, creating huge thrust.

344
00:17:19,890 --> 00:17:21,810
When we first started on the Shuttle

345
00:17:21,810 --> 00:17:26,622
our engines ran at, call it designed thrust, a 100%.

346
00:17:26,622 --> 00:17:28,740
(light dramatic music)

347
00:17:28,740 --> 00:17:32,103
Vehicle guys always want more power.

348
00:17:32,959 --> 00:17:36,220
(rocket engines blasting)

349
00:17:36,220 --> 00:17:37,290
Going to the SLS,

350
00:17:37,290 --> 00:17:40,651
the first flight will be at 109, not 100%.

351
00:17:40,651 --> 00:17:43,120
(rocket engines blasting)

352
00:17:43,120 --> 00:17:46,340
Eventually we're gonna go to higher power liberals, 111%.

353
00:17:46,340 --> 00:17:51,340
That's what NASA is aiming for is 111% of the rated power,

354
00:17:51,470 --> 00:17:54,991
which is quite a boost over the Shuttle era.

355
00:17:54,991 --> 00:17:58,320
(rocket engines blasting)

356
00:17:58,320 --> 00:18:01,010
In 2015 NASA begins testing

357
00:18:01,010 --> 00:18:04,943
all 16 RS-25 engines at the Stennis Space Center.

358
00:18:06,020 --> 00:18:09,340
It's a risky business pushing the engines to their limits

359
00:18:09,340 --> 00:18:12,206
and preparing them for their ultimate mission.

360
00:18:12,206 --> 00:18:15,460
(dramatic music)

361
00:18:15,460 --> 00:18:18,200
So, you know, in terms of increasing the thrust level

362
00:18:18,200 --> 00:18:19,400
of the RS-25 engine,

363
00:18:19,400 --> 00:18:21,270
we're increasing the mass that we're flowing,

364
00:18:21,270 --> 00:18:23,522
but we also increase the pressures that we see.

365
00:18:23,522 --> 00:18:24,840
(rocket engines blasting)

366
00:18:24,840 --> 00:18:26,440
If you start increasing pressures,

367
00:18:26,440 --> 00:18:28,390
then you also have higher temperatures.

368
00:18:29,420 --> 00:18:31,530
The turbo pumps have to be moving

369
00:18:31,530 --> 00:18:34,940
at faster rotational speeds.

370
00:18:34,940 --> 00:18:39,615
And you can imagine all of those things stress the material

371
00:18:39,615 --> 00:18:40,952
more and more.

372
00:18:40,952 --> 00:18:42,120
(rocket engines blasting)

373
00:18:42,120 --> 00:18:45,710
So it is that fine balance that dance, if you will,

374
00:18:45,710 --> 00:18:49,180
any change that you make affects not only the rocket engine,

375
00:18:49,180 --> 00:18:51,620
but it could affect the vehicle as a whole.

376
00:18:51,620 --> 00:18:55,037
(rocket engine blasting)

377
00:18:56,680 --> 00:18:57,720
For this vehicle, you know,

378
00:18:57,720 --> 00:19:02,010
it makes sense to make these engines expendable.

379
00:19:02,010 --> 00:19:03,210
The Space Shuttle main engine,

380
00:19:03,210 --> 00:19:06,720
or now the RS-25 was designed to be reusable.

381
00:19:06,720 --> 00:19:09,280
The Space Shuttle was that, it was a reusable vehicle:

382
00:19:09,280 --> 00:19:11,793
it went to low Earth orbit, it came back.

383
00:19:13,540 --> 00:19:15,840
The mission for SLS is different,

384
00:19:15,840 --> 00:19:18,163
we're going to the moon and beyond.

385
00:19:20,010 --> 00:19:22,310
So when we get to main engine cutoff,

386
00:19:22,310 --> 00:19:24,400
you're well out of the atmosphere,

387
00:19:24,400 --> 00:19:27,143
so there's really no way to bring those engines back.

388
00:19:28,230 --> 00:19:31,710
So you no longer have to design your engine

389
00:19:31,710 --> 00:19:33,313
for an extended life.

390
00:19:34,180 --> 00:19:36,210
And now that you have that shorter lifespan,

391
00:19:36,210 --> 00:19:39,860
then you could push your components to higher pressures,

392
00:19:39,860 --> 00:19:43,040
higher temperatures that may degrade its life.

393
00:19:43,040 --> 00:19:44,820
But since we're no longer we're reusing it,

394
00:19:44,820 --> 00:19:47,270
we're able to push those boundaries even farther.

395
00:19:48,980 --> 00:19:50,670
Those are the trades you have to make.

396
00:19:50,670 --> 00:19:55,070
We could not afford to carry the additional weight

397
00:19:55,070 --> 00:19:58,593
and complexity associated with reusability.

398
00:20:01,050 --> 00:20:04,113
But it hurts to throw away RS-25 engines.

399
00:20:05,121 --> 00:20:07,010
(upbeat music)

400
00:20:07,010 --> 00:20:08,640
I dunno how do you say it?

401
00:20:08,640 --> 00:20:10,010
It's a little bit disappointing,

402
00:20:10,010 --> 00:20:13,210
but we're going to the moon.

403
00:20:13,210 --> 00:20:17,140
I mean, if you're gonna be used for the last time

404
00:20:17,140 --> 00:20:20,200
in an expendable vehicle going to the moon,

405
00:20:20,200 --> 00:20:21,523
that's pretty cool.

406
00:20:22,726 --> 00:20:25,976
(deep pondering music)

407
00:20:46,520 --> 00:20:47,560
We wanna use those engines

408
00:20:47,560 --> 00:20:49,250
because no one's ever turned down

409
00:20:49,250 --> 00:20:50,790
high thrust and high fuel economy.

410
00:20:50,790 --> 00:20:53,157
Nobody's ever said, "Oh, I don't want those things

411
00:20:53,157 --> 00:20:53,997
"on a rocket."

412
00:20:56,940 --> 00:20:59,340
And that drives this requirement

413
00:20:59,340 --> 00:21:01,263
of having these cryogenic propellants.

414
00:21:02,940 --> 00:21:04,710
Hydrogen is the most efficient

415
00:21:04,710 --> 00:21:06,640
known rocket propellant,

416
00:21:06,640 --> 00:21:08,393
but it has a very low density.

417
00:21:09,320 --> 00:21:12,240
Storing it and the oxygen needed to burn it,

418
00:21:12,240 --> 00:21:15,600
even in liquid form requires huge tanks

419
00:21:15,600 --> 00:21:17,073
and very low temperatures.

420
00:21:18,140 --> 00:21:21,723
Any leakage creates a risk of catastrophic explosion.

421
00:21:22,600 --> 00:21:24,760
When you liquefy them you can carry a lot more

422
00:21:24,760 --> 00:21:27,050
in a smaller space, but if they get too warm

423
00:21:27,050 --> 00:21:31,663
they flash to gas immediately, and then you're in trouble.

424
00:21:34,130 --> 00:21:36,620
It's just not a normal part of engineering

425
00:21:36,620 --> 00:21:38,530
to do cryogenic engineering.

426
00:21:38,530 --> 00:21:41,660
We don't normally, in our everyday life, do things

427
00:21:41,660 --> 00:21:44,363
that are at 40 degrees above absolute zero.

428
00:21:47,100 --> 00:21:51,490
The hydrogen is so cold that it will actually freeze

429
00:21:51,490 --> 00:21:55,030
the air around it in a duct, for instance.

430
00:21:55,030 --> 00:21:58,000
So we have to make sure that we've got the proper insulation

431
00:21:58,000 --> 00:21:59,770
on the ducting, not just on our engines,

432
00:21:59,770 --> 00:22:01,070
but throughout the system.

433
00:22:03,350 --> 00:22:08,133
Cryogenic temperatures can wreak havoc on components.

434
00:22:10,200 --> 00:22:14,240
Large metal structures, valves, when you hit them

435
00:22:15,173 --> 00:22:18,750
with cryogenic oxygen or hydrogen they change,

436
00:22:18,750 --> 00:22:20,533
they move, they shrink.

437
00:22:22,210 --> 00:22:25,820
The tank itself wants to expand with pressure,

438
00:22:25,820 --> 00:22:28,090
it wants to shrink with the cryogenic,

439
00:22:28,090 --> 00:22:32,270
and so all of that goes into designing hardware

440
00:22:32,270 --> 00:22:34,810
for the SLS program.

441
00:22:34,810 --> 00:22:37,393
(upbeat music)

442
00:22:40,440 --> 00:22:41,730
The tanks need to stand up

443
00:22:41,730 --> 00:22:44,540
to more than just changes in temperature,

444
00:22:44,540 --> 00:22:46,310
they also need to withstand

445
00:22:46,310 --> 00:22:49,673
the 8.8 million pounds of thrust at launch.

446
00:22:50,920 --> 00:22:54,310
It's one thing to know that you have a strong structure,

447
00:22:54,310 --> 00:22:56,550
it's another thing to take such a massive structure

448
00:22:56,550 --> 00:22:57,383
and test it.

449
00:22:59,270 --> 00:23:02,770
You don't build a scale model, you build a piece of hardware

450
00:23:02,770 --> 00:23:04,670
that's like flight.

451
00:23:04,670 --> 00:23:06,980
You know, the desire is to build it as if it could be

452
00:23:06,980 --> 00:23:09,480
just interchanged with a piece of flight hardware.

453
00:23:10,520 --> 00:23:12,810
We're looking at simulating the different loads

454
00:23:12,810 --> 00:23:15,680
that it would undergo during flight.

455
00:23:15,680 --> 00:23:18,130
You want to know that as you designed it

456
00:23:18,130 --> 00:23:21,360
it will be able to carry out all of the different loads

457
00:23:21,360 --> 00:23:24,393
and still maintain its structural integrity.

458
00:23:24,393 --> 00:23:27,670
(pondering music)

459
00:23:27,670 --> 00:23:29,150
It said in NASA

460
00:23:29,150 --> 00:23:34,010
that they work for a 1.4 factor of safety,

461
00:23:34,010 --> 00:23:37,330
meaning that something, a rocket should be able to tolerate

462
00:23:37,330 --> 00:23:39,630
a load about one and a half higher

463
00:23:39,630 --> 00:23:41,280
than what they think is possible.

464
00:23:42,850 --> 00:23:46,980
For factors of safety as high as 11 for elevator cables,

465
00:23:46,980 --> 00:23:50,370
airplanes factor of 2, 2 1/5,

466
00:23:50,370 --> 00:23:53,430
so you could say of all the devices that mankind has made

467
00:23:53,430 --> 00:23:56,120
rockets have about the narrowest factor of safety

468
00:23:56,120 --> 00:23:58,860
because you need to have everything kind of running

469
00:23:58,860 --> 00:24:01,033
right on the ragged edge.

470
00:24:03,150 --> 00:24:05,250
If you don't, it won't get off the ground.

471
00:24:06,680 --> 00:24:09,180
Confirming the design is neither too strong

472
00:24:09,180 --> 00:24:12,110
nor too weak means testing it to destruction

473
00:24:12,110 --> 00:24:14,913
in a giant rig to simulate the load in flight.

474
00:24:16,890 --> 00:24:19,740
It needs to break exactly as predicted.

475
00:24:19,740 --> 00:24:21,340
It was a pneumatic test.

476
00:24:21,340 --> 00:24:23,460
We're pushing down on this tank

477
00:24:23,460 --> 00:24:25,286
while we have pressure on it.

478
00:24:25,286 --> 00:24:27,720
(light anticipatory music)

479
00:24:27,720 --> 00:24:29,410
You hold your breath.

480
00:24:29,410 --> 00:24:32,510
(light anticipatory music)

481
00:24:32,510 --> 00:24:35,160
The first thing that we heard was an audible noise.

482
00:24:36,079 --> 00:24:39,079
(engines exploding)

483
00:24:41,200 --> 00:24:43,950
Did what we thought it would do it buckled.

484
00:24:43,950 --> 00:24:45,543
And we actually clapped.

485
00:24:47,780 --> 00:24:50,910
The models work really well, I was ready to call it a day.

486
00:24:50,910 --> 00:24:52,160
You know, we'd tested the tank

487
00:24:52,160 --> 00:24:54,490
that's when it breaks in flight.

488
00:24:54,490 --> 00:24:56,823
But the tank held one last surprise.

489
00:24:57,694 --> 00:24:59,100
(tank exploding)

490
00:24:59,100 --> 00:25:02,140
We had high speed video of this metal

491
00:25:02,140 --> 00:25:05,100
that's more than a half inch thick flopping in the breeze,

492
00:25:05,100 --> 00:25:06,229
like a feather.

493
00:25:06,229 --> 00:25:08,570
(steam sizzling)

494
00:25:08,570 --> 00:25:11,490
After spending so much time welding

495
00:25:11,490 --> 00:25:14,520
all of the tanks together in such a precise manner,

496
00:25:14,520 --> 00:25:18,610
actually seeing it break apart can kind of cause your heart

497
00:25:18,610 --> 00:25:20,180
to break, to be honest.

498
00:25:20,180 --> 00:25:22,630
But it's very important data that we need

499
00:25:22,630 --> 00:25:25,970
in order to understand the true capability

500
00:25:25,970 --> 00:25:27,963
of the structural test article.

501
00:25:29,152 --> 00:25:32,680
(light upbeat music)

502
00:25:32,680 --> 00:25:36,150
The oxygen tank we tested was very similar.

503
00:25:36,150 --> 00:25:38,350
We wanted to test that oxygen tank

504
00:25:38,350 --> 00:25:39,780
at reasonably high pressure.

505
00:25:39,780 --> 00:25:42,610
And to do that pneumatically would produced so much energy

506
00:25:42,610 --> 00:25:47,230
that it would hurt the test stand and be a danger to folks,

507
00:25:47,230 --> 00:25:49,143
and so we filled it full of water.

508
00:25:50,024 --> 00:25:52,941
(pondering music)

509
00:26:08,580 --> 00:26:10,493
I liked those test to failures.

510
00:26:12,230 --> 00:26:15,370
The reason by the way we test to failure is to see

511
00:26:15,370 --> 00:26:16,880
how much margin we have.

512
00:26:16,880 --> 00:26:18,770
And it turned out in that hydrogen tank,

513
00:26:18,770 --> 00:26:21,156
we have tremendous margin.

514
00:26:21,156 --> 00:26:24,610
(dramatic music)

515
00:26:24,610 --> 00:26:27,633
The core stage has aced its structural tests.

516
00:26:29,270 --> 00:26:31,530
Now all the segments must be joined together

517
00:26:31,530 --> 00:26:34,103
with its four RS-25 engines.

518
00:26:36,130 --> 00:26:38,650
But despite the engine's awesome power,

519
00:26:38,650 --> 00:26:41,300
not even pushing them past their design limit

520
00:26:41,300 --> 00:26:45,395
will create enough thrust to get SLS off the planet.

521
00:26:45,395 --> 00:26:46,580
(dramatic music)

522
00:26:46,580 --> 00:26:50,480
My most efficient fuel, it turns out is hydrogen,

523
00:26:50,480 --> 00:26:53,640
it gives me very high exhaust velocities.

524
00:26:53,640 --> 00:26:56,810
And now that part of my rocket equation is satisfied,

525
00:26:56,810 --> 00:26:59,290
it loves hydrogen.

526
00:26:59,290 --> 00:27:02,980
But hydrogen is such a low density that now I've got to have

527
00:27:02,980 --> 00:27:05,380
this huge tank to hold it.

528
00:27:05,380 --> 00:27:06,213
And guess what?

529
00:27:06,213 --> 00:27:08,584
My dry weight has gone up.

530
00:27:08,584 --> 00:27:11,130
(upbeat music)

531
00:27:11,130 --> 00:27:14,480
I need Solid Rocket Boosters to help get that big tank

532
00:27:14,480 --> 00:27:15,313
off the ground.

533
00:27:16,186 --> 00:27:18,580
(upbeat music)

534
00:27:18,580 --> 00:27:20,540
The current booster is a derivation

535
00:27:20,540 --> 00:27:24,190
from the Space Shuttle and it does look on the outside,

536
00:27:24,190 --> 00:27:25,880
very similar to the Space Shuttle Booster,

537
00:27:25,880 --> 00:27:30,490
but it is 25% longer, has 25% more fuel to provide

538
00:27:30,490 --> 00:27:31,913
that much more thrust.

539
00:27:33,380 --> 00:27:35,790
Each booster is built from five segments

540
00:27:35,790 --> 00:27:37,913
filled with a solid epoxy propellant.

541
00:27:40,390 --> 00:27:43,850
Once stuck together the segments stand 17 stories tall

542
00:27:43,850 --> 00:27:47,083
and create more trust than 14 jumbo jets.

543
00:27:48,090 --> 00:27:50,390
I like to think of the boosters is an afterburner

544
00:27:50,390 --> 00:27:51,940
on a fighter jet.

545
00:27:51,940 --> 00:27:55,590
When you have a heavy rocket lifting off of the launch pad,

546
00:27:55,590 --> 00:27:57,460
over 90% of that is fuel.

547
00:27:57,460 --> 00:28:00,580
And so you have to have an immense amount of thrust

548
00:28:00,580 --> 00:28:02,780
to get that off the ground.

549
00:28:02,780 --> 00:28:04,870
(rocket engines blasting)

550
00:28:04,870 --> 00:28:08,260
SLS generates over 8 million pounds of thrust

551
00:28:08,260 --> 00:28:09,950
and the Solid Rocket Boosters

552
00:28:09,950 --> 00:28:12,957
generate about 5 million pounds of that by itself.

553
00:28:12,957 --> 00:28:14,440
(rocket engines blasting)

554
00:28:14,440 --> 00:28:16,850
So the boosters contribute the majority

555
00:28:16,850 --> 00:28:20,090
of the thrust capability for SLS.

556
00:28:20,090 --> 00:28:22,170
When I flew Space Shuttles, I could feel that

557
00:28:22,170 --> 00:28:26,490
in the crew module as this incredible push.

558
00:28:26,490 --> 00:28:31,240
(dramatic music)
(rocket engines blasting)

559
00:28:31,240 --> 00:28:35,100
Even though its efficiency is not as good as hydrogen,

560
00:28:35,100 --> 00:28:38,220
it burns propellant with very high thrust

561
00:28:39,206 --> 00:28:41,900
and it loses its weight very rapidly,

562
00:28:41,900 --> 00:28:45,703
and so I can accelerate the vehicle coming off of the pad.

563
00:28:45,703 --> 00:28:50,703
(rocket engines blasting)
(dramatic music)

564
00:28:56,460 --> 00:28:59,540
You want to dump weight as fast as you can.

565
00:28:59,540 --> 00:29:03,650
And so what we do is when we empty a stage of fuel,

566
00:29:03,650 --> 00:29:06,630
it's no good to us anymore, it's dry weight.

567
00:29:06,630 --> 00:29:09,439
We release it and let it drop into the ocean.

568
00:29:09,439 --> 00:29:12,939
(rocket engines blasting)

569
00:29:16,420 --> 00:29:21,393
Five, four, three, two, one, fire.

570
00:29:23,160 --> 00:29:25,360
Work on converting the Solid Rocket Boosters

571
00:29:25,360 --> 00:29:28,003
for SLS began back in 2013,

572
00:29:28,910 --> 00:29:31,967
with testing carried out in Promontory, Utah.

573
00:29:31,967 --> 00:29:33,900
You've got 10 seconds.

574
00:29:33,900 --> 00:29:36,830
Once we lift off, we're now confronted with

575
00:29:36,830 --> 00:29:40,550
a lot of challenges that we have to have designed properly.

576
00:29:40,550 --> 00:29:42,000
Chief has 20 seconds.

577
00:29:42,000 --> 00:29:44,660
The temperature that the Solid Rocket fuels burn at

578
00:29:44,660 --> 00:29:48,760
is in excess of 5,000, pushing 6,000 degrees.

579
00:29:48,760 --> 00:29:51,210
And what we do is we ignite it from the top

580
00:29:51,210 --> 00:29:53,712
and we let it burn out the bottom in a nozzle.

581
00:29:53,712 --> 00:29:56,460
(fire blasting)

582
00:29:56,460 --> 00:30:00,380
And you have this tube of propellant that joins up

583
00:30:00,380 --> 00:30:02,029
with a steel casing.

584
00:30:02,029 --> 00:30:03,757
You've got 30 seconds.

585
00:30:03,757 --> 00:30:06,520
You don't just put the propellant next to the steel,

586
00:30:06,520 --> 00:30:07,623
that would melt it.

587
00:30:09,300 --> 00:30:12,780
So there has to be an insulating rubber layer

588
00:30:12,780 --> 00:30:16,783
that protects the steel from that intense flame.

589
00:30:18,910 --> 00:30:22,150
In the Shuttle system we had an asbestos fiber

590
00:30:22,150 --> 00:30:24,590
that was effective, but not as effective

591
00:30:24,590 --> 00:30:26,023
as these new materials.

592
00:30:27,100 --> 00:30:31,370
That rubber insulation, as it is exposed to heat

593
00:30:31,370 --> 00:30:34,840
actually turns to a charred material that further protects

594
00:30:34,840 --> 00:30:37,443
the case from any exposure to the heat.

595
00:30:38,328 --> 00:30:40,230
(rocket engines blasting)

596
00:30:40,230 --> 00:30:43,980
NASA worries about voids between the propellant

597
00:30:43,980 --> 00:30:45,693
and that rubber liner.

598
00:30:46,740 --> 00:30:49,750
That could cause an extra point of heat

599
00:30:49,750 --> 00:30:51,883
as that propellant burns down.

600
00:30:52,900 --> 00:30:55,109
The consequences of that could be improper burning,

601
00:30:55,109 --> 00:30:59,140
could be early burn back through the insulation,

602
00:30:59,140 --> 00:31:00,930
which is not something you wanna deal with

603
00:31:00,930 --> 00:31:04,120
when you're talking about the massive forces

604
00:31:04,120 --> 00:31:06,065
inside a rocket motor.

605
00:31:06,065 --> 00:31:06,898
(dramatic music)

606
00:31:06,898 --> 00:31:08,590
Even the tiniest void could cause

607
00:31:08,590 --> 00:31:10,770
a catastrophic failure at lunch.

608
00:31:10,770 --> 00:31:14,270
We eventually got to processes that could eliminate

609
00:31:14,270 --> 00:31:17,090
those voids and it took an immense amount of engineering

610
00:31:17,090 --> 00:31:18,530
to do that.

611
00:31:18,530 --> 00:31:20,590
The Solid Rocket Boosters will operate

612
00:31:20,590 --> 00:31:23,700
for just 126 seconds at flight.

613
00:31:23,700 --> 00:31:26,443
And within that the first minute is crucial.

614
00:31:27,469 --> 00:31:29,219
You've got 40 seconds.

615
00:31:30,310 --> 00:31:32,370
30 to 50 seconds after liftoff,

616
00:31:32,370 --> 00:31:34,970
you start to approach this transonic regime

617
00:31:34,970 --> 00:31:36,959
where shock waves form.

618
00:31:36,959 --> 00:31:39,520
(dramatic music)
(rocket engines blasting)

619
00:31:39,520 --> 00:31:41,910
Max-Q, max dynamic pressure.

620
00:31:41,910 --> 00:31:43,470
There's nobody in this industry

621
00:31:43,470 --> 00:31:46,314
that doesn't think about Max-Q.

622
00:31:46,314 --> 00:31:49,222
(rocket engines blasting)

623
00:31:49,222 --> 00:31:50,690
And if you didn't throttle back,

624
00:31:50,690 --> 00:31:52,753
you could do damage to the structure.

625
00:31:52,753 --> 00:31:53,840
(dramatic music)

626
00:31:53,840 --> 00:31:56,630
The boosters use a clever trick to throttle back

627
00:31:56,630 --> 00:31:58,163
and then build trust again,

628
00:31:59,490 --> 00:32:02,020
and it's baked into the design.

629
00:32:02,020 --> 00:32:05,750
We put fins into that propellant,

630
00:32:05,750 --> 00:32:10,190
so as you look down you actually see a star shape pattern,

631
00:32:10,190 --> 00:32:13,350
and all of that pattern is exposed propellant.

632
00:32:13,350 --> 00:32:17,030
And it turns out that the rate at which the propellant burns

633
00:32:17,030 --> 00:32:20,639
is proportional to how much propellant is exposed.

634
00:32:20,639 --> 00:32:24,139
(rocket engines blasting)

635
00:32:26,220 --> 00:32:28,940
And we time that such that as the rocket reaches

636
00:32:28,940 --> 00:32:31,350
this point of maximum dynamic pressure,

637
00:32:31,350 --> 00:32:35,140
we're actually throttling the Solid Rocket Booster

638
00:32:35,140 --> 00:32:36,800
to where the thrust decreases

639
00:32:36,800 --> 00:32:38,310
till we break through that sound barrier,

640
00:32:38,310 --> 00:32:40,006
we push it back again.

641
00:32:40,006 --> 00:32:43,506
(rocket engines blasting)

642
00:32:44,803 --> 00:32:47,205
You've got 120 seconds.

643
00:32:47,205 --> 00:32:50,705
(rocket engines blasting)

644
00:32:54,320 --> 00:32:56,070
Activate head and CO2.

645
00:32:58,600 --> 00:33:02,380
(train horn blasting)

646
00:33:02,380 --> 00:33:03,880
Because the booster is so large

647
00:33:03,880 --> 00:33:06,790
we actually ship it in separate segments by train

648
00:33:07,860 --> 00:33:10,390
from the manufacturing facility in Utah

649
00:33:10,390 --> 00:33:12,140
to the launch site at Cape Kennedy,

650
00:33:12,140 --> 00:33:13,813
and at the Kennedy Space Center.

651
00:33:16,289 --> 00:33:18,603
(light dramatic music)

652
00:33:18,603 --> 00:33:21,650
The Vehicle Assembly Building or VAB as we refer to it,

653
00:33:21,650 --> 00:33:26,140
it's a single-story building, but it's huge, 525 feet tall.

654
00:33:26,140 --> 00:33:29,136
We could build four rockets at a time if we really wanted.

655
00:33:29,136 --> 00:33:30,050
(dramatic music)

656
00:33:30,050 --> 00:33:32,210
The arrival of the Solid Rocket Boosters

657
00:33:32,210 --> 00:33:35,840
sets off an irreversible countdown to lunch.

658
00:33:35,840 --> 00:33:38,110
Once they are assembled they must be used

659
00:33:38,110 --> 00:33:40,640
within 12 months before there are damaged

660
00:33:40,640 --> 00:33:42,460
by their own weight.

661
00:33:42,460 --> 00:33:45,150
There is a timeframe here that we've got to march to,

662
00:33:45,150 --> 00:33:48,600
we've got to steadily make progress, we have a plan.

663
00:33:48,600 --> 00:33:49,900
With time critical,

664
00:33:49,900 --> 00:33:51,970
nothing has been left to chance.

665
00:33:51,970 --> 00:33:55,140
The entire procedure has been planned and rehearsed

666
00:33:55,140 --> 00:33:57,019
for every part of SLS.

667
00:33:57,019 --> 00:33:58,460
(dramatic music)

668
00:33:58,460 --> 00:33:59,900
I don't care how much experience you have,

669
00:33:59,900 --> 00:34:00,950
this rocket is new.

670
00:34:00,950 --> 00:34:02,973
So we train our folks all the time.

671
00:34:04,080 --> 00:34:07,710
Brought a mock-up of the entire 212-foot long

672
00:34:07,710 --> 00:34:10,013
rocket stage pathfinder, we called it,

673
00:34:11,170 --> 00:34:14,130
and we let our people rotate it, handle it,

674
00:34:14,130 --> 00:34:16,732
lift it and practice with it.

675
00:34:16,732 --> 00:34:19,565
(dramatic music)

676
00:34:21,822 --> 00:34:23,700
One of the biggest things that we had to consider,

677
00:34:23,700 --> 00:34:28,123
in the design of the SLS was its attachment to the ground.

678
00:34:29,560 --> 00:34:31,490
NASA began essential upgrades

679
00:34:31,490 --> 00:34:35,023
to the Kennedy Space Center's facilities back in 2013.

680
00:34:36,020 --> 00:34:39,750
For SLS it has revolutionized one iconic idea

681
00:34:39,750 --> 00:34:44,486
from the Saturn V program, Launch Umbilical Tower.

682
00:34:44,486 --> 00:34:47,470
(dramatic music)

683
00:34:47,470 --> 00:34:50,030
This is a massive, massive structure

684
00:34:50,030 --> 00:34:51,290
that when you're at the top of it

685
00:34:51,290 --> 00:34:53,240
you're roughly 400 feet off the ground.

686
00:34:55,930 --> 00:34:59,100
The structure was built for the Constellation program,

687
00:34:59,100 --> 00:35:01,150
but then, that's about as far as we got,

688
00:35:01,150 --> 00:35:03,050
because then the program was canceled.

689
00:35:05,090 --> 00:35:07,197
It saved us money to go ahead and say,

690
00:35:07,197 --> 00:35:09,987
"Okay, let's transform this mobile launcher

691
00:35:09,987 --> 00:35:12,267
"from Constellation over here to SLS."

692
00:35:13,320 --> 00:35:15,173
Now, sounds straightforward, right.

693
00:35:16,200 --> 00:35:18,420
But, honestly, when you look at SLS,

694
00:35:18,420 --> 00:35:20,730
the weight is tremendously increased,

695
00:35:20,730 --> 00:35:24,110
the power of the rocket is tremendously increased.

696
00:35:24,110 --> 00:35:26,810
So we had to basically reinforce the entire structure.

697
00:35:30,580 --> 00:35:33,490
The umbilicals provide, you know, the food if you will,

698
00:35:33,490 --> 00:35:35,440
the carrying and feeding to the rocket,

699
00:35:36,466 --> 00:35:39,330
the fuel, the gasses, the cooling, the communications,

700
00:35:39,330 --> 00:35:42,210
the data all feed through these arms that are attached

701
00:35:42,210 --> 00:35:44,770
to the giant tower on the mobile launcher.

702
00:35:44,770 --> 00:35:49,500
When we fire the SRBs, the Solid Rocket Boosters,

703
00:35:49,500 --> 00:35:52,170
we're basically moving within a quarter of a second.

704
00:35:52,170 --> 00:35:55,423
So literally within a blink of an eye,

705
00:35:55,423 --> 00:35:57,545
(rocket engines blasting)

706
00:35:57,545 --> 00:35:59,410
the mobile launcher platform has to release

707
00:35:59,410 --> 00:36:02,200
all of those umbilicals and get back out of the way

708
00:36:02,200 --> 00:36:04,773
of the vehicle as the vehicle rises off the pad.

709
00:36:05,862 --> 00:36:08,695
(dramatic music)

710
00:36:13,360 --> 00:36:15,770
She throw us a curve ball every day.

711
00:36:15,770 --> 00:36:17,610
It was a tough process.

712
00:36:17,610 --> 00:36:21,240
I spent, you know, three and a half years out there,

713
00:36:21,240 --> 00:36:22,740
basically living in a trailer.

714
00:36:22,740 --> 00:36:24,470
But when you're working on something like that,

715
00:36:24,470 --> 00:36:26,660
you realize it's unique, it's one.

716
00:36:26,660 --> 00:36:28,160
You know what you're doing with it, right

717
00:36:28,160 --> 00:36:30,853
I'm gonna launch the world's most powerful rocket.

718
00:36:30,853 --> 00:36:33,023
So all of that helps drive you.

719
00:36:34,620 --> 00:36:36,770
The tower sits on top of a platform

720
00:36:36,770 --> 00:36:38,763
over 21,000 feet square.

721
00:36:40,490 --> 00:36:42,783
Together they form the mobile launcher.

722
00:36:44,750 --> 00:36:47,540
The mobile launcher or ML as we always refer to it

723
00:36:47,540 --> 00:36:50,880
is, essentially, the cradle, it's kind of the central point

724
00:36:50,880 --> 00:36:53,325
of assembling and testing the rocket.

725
00:36:53,325 --> 00:36:56,075
(dramatic music)

726
00:36:57,753 --> 00:36:59,490
The entire rocket will be built on top

727
00:36:59,490 --> 00:37:01,930
of the mobile launcher, and then the mobile launcher

728
00:37:01,930 --> 00:37:05,943
is transferred out to the pad using the Crawler-transporter.

729
00:37:09,500 --> 00:37:13,020
We do have a season for hurricanes, that can be tough.

730
00:37:13,020 --> 00:37:14,380
If we were out at the pad,

731
00:37:14,380 --> 00:37:16,140
when a hurricane were to come along,

732
00:37:16,140 --> 00:37:18,700
we would roll back to the VAB and button the rocket up

733
00:37:18,700 --> 00:37:20,807
inside there and ride it out.

734
00:37:20,807 --> 00:37:23,640
(pondering music)

735
00:37:27,522 --> 00:37:30,605
(anticipatory music)

736
00:37:34,920 --> 00:37:36,810
Stacking the Solid Rocket Boosters

737
00:37:36,810 --> 00:37:38,820
is progressing well.

738
00:37:38,820 --> 00:37:41,180
Now the pressure is on to get the core stage

739
00:37:41,180 --> 00:37:43,386
to the vehicle assembly building.

740
00:37:43,386 --> 00:37:46,250
(anticipatory music)

741
00:37:46,250 --> 00:37:49,280
But first the entire stage must be lifted into a stand

742
00:37:49,280 --> 00:37:53,563
at the Stennis Space Center for a crucial hot fire test.

743
00:37:54,839 --> 00:37:58,160
(anticipatory music)

744
00:37:58,160 --> 00:38:00,290
The weight of that column of liquid pushing down

745
00:38:00,290 --> 00:38:02,540
on the engines at the bottom creates

746
00:38:02,540 --> 00:38:05,403
a different operating condition when the engines start.

747
00:38:06,445 --> 00:38:07,278
(anticipatory music)

748
00:38:07,278 --> 00:38:09,220
The problem we could have had with the engine

749
00:38:09,220 --> 00:38:12,120
was a structural failure.

750
00:38:12,120 --> 00:38:13,893
So we had to go prove on the test stand

751
00:38:13,893 --> 00:38:16,800
that the engine would start and run

752
00:38:16,800 --> 00:38:19,943
at liquid oxygen pressures that high.

753
00:38:22,098 --> 00:38:23,320
(pondering music)

754
00:38:23,320 --> 00:38:27,100
It is primarily a test of the propulsion systems,

755
00:38:27,100 --> 00:38:30,740
and so there's a lot of focus on my hardware,

756
00:38:30,740 --> 00:38:33,833
which is the steering system for the rocket.

757
00:38:34,940 --> 00:38:36,980
Space Launch System will be steered

758
00:38:36,980 --> 00:38:40,030
using a technique known as gimballing.

759
00:38:40,030 --> 00:38:42,670
It requires precise individual adjustments

760
00:38:42,670 --> 00:38:46,090
to the direction of the four RS-25 engines.

761
00:38:46,090 --> 00:38:50,010
You're trying to make adjustments of less than a degree

762
00:38:50,010 --> 00:38:53,300
sometimes in those nozzles to change the trajectory

763
00:38:53,300 --> 00:38:56,430
just slightly on a vehicle that is going

764
00:38:56,430 --> 00:38:59,890
thousands of miles per hour through the atmosphere.

765
00:38:59,890 --> 00:39:04,560
And they have to work perfectly every single time

766
00:39:04,560 --> 00:39:08,563
because there is no room for error in steering the rocket.

767
00:39:10,850 --> 00:39:12,050
We designed these parts

768
00:39:12,050 --> 00:39:13,840
and they're supposed to do a certain thing,

769
00:39:13,840 --> 00:39:16,933
but you never know until you actually test.

770
00:39:19,460 --> 00:39:21,930
The ultimate test is the hot fire test,

771
00:39:21,930 --> 00:39:25,560
and that is where all four engines are firing

772
00:39:25,560 --> 00:39:27,023
for a simulated flight.

773
00:39:29,000 --> 00:39:31,500
The only difference is that the core stage

774
00:39:31,500 --> 00:39:33,463
is bolted into a test stand.

775
00:39:36,460 --> 00:39:39,210
Everything is there to mimic the launch

776
00:39:39,210 --> 00:39:40,470
as just the core stage alone.

777
00:39:40,470 --> 00:39:43,180
So you actually have to fool the rocket into thinking

778
00:39:43,180 --> 00:39:44,363
there's boosters there.

779
00:39:45,900 --> 00:39:50,050
Firing a Solid Rocket Booster in that kind of position

780
00:39:50,050 --> 00:39:52,203
we would have melted the test stand down.

781
00:39:53,253 --> 00:39:56,340
(pondering music)

782
00:39:56,340 --> 00:40:01,340
We need to test all the engines for at least four minutes

783
00:40:01,620 --> 00:40:02,630
if not eight minutes.

784
00:40:02,630 --> 00:40:04,313
Eight minutes is a full flight.

785
00:40:05,378 --> 00:40:08,211
(pondering music)

786
00:40:11,550 --> 00:40:13,050
This is the last major hurdle

787
00:40:13,050 --> 00:40:15,430
in making its way towards the launch pad.

788
00:40:15,430 --> 00:40:19,410
It's a kind of test, you know, comes along once in a career,

789
00:40:19,410 --> 00:40:21,963
once in a lifetime.

790
00:40:23,430 --> 00:40:25,120
I'm in the test control center

791
00:40:25,120 --> 00:40:27,243
with the steel blast doors closed.

792
00:40:30,220 --> 00:40:35,220
10, 9, 8, 7,
(rocket engines blasting)

793
00:40:35,538 --> 00:40:39,237
and you see the steam and the fire coming out of this hole.

794
00:40:39,237 --> 00:40:42,737
(rocket engines blasting)

795
00:40:44,179 --> 00:40:46,802
And we're (indistinct), engine start.

796
00:40:46,802 --> 00:40:48,630
When those engines start up,

797
00:40:48,630 --> 00:40:52,120
even though you're locked inside a bunker,

798
00:40:52,120 --> 00:40:55,300
you can still feel the power of four engines running

799
00:40:55,300 --> 00:40:56,632
at the same time.

800
00:40:56,632 --> 00:41:00,132
(rocket engines blasting)

801
00:41:03,250 --> 00:41:05,715
All right less 25 seconds.

802
00:41:05,715 --> 00:41:07,563
(rocket engines blasting)

803
00:41:07,563 --> 00:41:10,829
PDRA we did get an MCF on engine four.

804
00:41:10,829 --> 00:41:13,160
Roger that, but we're still running.

805
00:41:13,160 --> 00:41:13,993
We've still got four-

806
00:41:13,993 --> 00:41:15,668
There's a couple of things going on

807
00:41:15,668 --> 00:41:17,450
that you didn't exactly predict,

808
00:41:17,450 --> 00:41:20,701
but actually it didn't affect our rocket at all, you know.

809
00:41:20,701 --> 00:41:23,470
(dramatic music)
(rocket engines blasting)

810
00:41:23,470 --> 00:41:24,890
Things were going well.

811
00:41:24,890 --> 00:41:28,242
We were just starting the first gimbal test.

812
00:41:28,242 --> 00:41:31,742
(rocket engines blasting)

813
00:41:32,670 --> 00:41:35,875
You see these engines and they look like they're dancing.

814
00:41:35,875 --> 00:41:38,230
(rocket engines blasting)

815
00:41:38,230 --> 00:41:40,220
We got 62 seconds into test

816
00:41:42,020 --> 00:41:43,592
and we shut down.

817
00:41:43,592 --> 00:41:44,680
(indistinct)

818
00:41:44,680 --> 00:41:45,933
Gotcha.

819
00:41:45,933 --> 00:41:47,687
(indistinct) safety violation (indistinct).

820
00:41:49,370 --> 00:41:54,370
There was an announcement, major component malfunction.

821
00:41:54,444 --> 00:41:57,944
(rocket engines blasting)

822
00:41:59,160 --> 00:42:03,940
And in that moment, you kind of feel the light shift

823
00:42:03,940 --> 00:42:05,583
in your direction a little bit.

824
00:42:07,350 --> 00:42:08,183
What did I miss?

825
00:42:08,183 --> 00:42:09,840
What did I not see?

826
00:42:09,840 --> 00:42:12,870
Certainly all of that is going through your mind.

827
00:42:12,870 --> 00:42:16,180
Rockets operate on such a very narrow margin

828
00:42:16,180 --> 00:42:20,500
that when something is called a major component malfunction,

829
00:42:20,500 --> 00:42:22,878
you sit up and take notice.

830
00:42:22,878 --> 00:42:24,390
{\an8}(indistinct) personnel.

831
00:42:24,390 --> 00:42:25,430
{\an8}Shut down looks like

832
00:42:25,430 --> 00:42:28,523
{\an8}let's all go to page 656, page 656, please.

833
00:42:30,860 --> 00:42:33,910
{\an8}When something like that occurs and you shut down,

834
00:42:33,910 --> 00:42:36,230
the first thing you're doing is just securing the hardware.

835
00:42:36,230 --> 00:42:38,460
You know, we've got flight hardware sitting on the pad

836
00:42:38,460 --> 00:42:40,670
{\an8}and it still has cryogenics in it.

837
00:42:40,670 --> 00:42:43,650
{\an8}The best way to drain the tank is to burn for eight minutes

838
00:42:43,650 --> 00:42:45,960
and then I don't have those cryogenics in it,

839
00:42:45,960 --> 00:42:49,020
but I've got cryogenics that's really, really cold,

840
00:42:49,020 --> 00:42:51,610
and then I've got an engine that's really, really hot,

841
00:42:51,610 --> 00:42:54,942
and I wanna make sure all of those systems are safe.

842
00:42:54,942 --> 00:42:56,260
All personnel it's gonna be

843
00:42:56,260 --> 00:42:58,490
post hot-fire shut down securing operations

844
00:42:58,490 --> 00:42:59,980
in page 656.

845
00:42:59,980 --> 00:43:04,980
At this point, the core stage is a golden egg for NASA.

846
00:43:06,060 --> 00:43:09,250
Meaning there is nothing else on the shelf

847
00:43:09,250 --> 00:43:10,453
that can replace it.

848
00:43:11,960 --> 00:43:14,470
If something happened that broke the egg,

849
00:43:14,470 --> 00:43:17,000
that could be the end of mission event.

850
00:43:17,000 --> 00:43:18,560
AR1 (indistinct) please verify

851
00:43:18,560 --> 00:43:20,540
we have a safe engine shutdown.

852
00:43:20,540 --> 00:43:21,470
We are in post shutdown,

853
00:43:21,470 --> 00:43:24,770
standby, engine 1 through 4.

854
00:43:24,770 --> 00:43:28,443
It took a good hour to figure out what went wrong.

855
00:43:29,310 --> 00:43:31,700
For this first test NASA has set

856
00:43:31,700 --> 00:43:34,833
very tight limits to avoid damaging the flight hardware.

857
00:43:35,760 --> 00:43:37,800
One limit has been reached.

858
00:43:37,800 --> 00:43:40,760
But after carefully reviewing all the gathered data

859
00:43:40,760 --> 00:43:43,590
engineers determined that it can be safely relaxed

860
00:43:43,590 --> 00:43:44,873
ahead of a new test.

861
00:43:45,900 --> 00:43:47,567
You know, people misunderstand tests,

862
00:43:47,567 --> 00:43:49,600
they're not stunts, they're not media events,

863
00:43:49,600 --> 00:43:51,980
what they are is they're answers to questions

864
00:43:51,980 --> 00:43:53,020
that you had.

865
00:43:53,020 --> 00:43:55,080
You're looking at the historic

866
00:43:55,080 --> 00:43:57,013
B Test Complex at NASA's-

867
00:43:57,930 --> 00:43:59,520
So for the second hot fire,

868
00:43:59,520 --> 00:44:02,130
we recognized that both the media,

869
00:44:02,130 --> 00:44:05,190
and really the eyes within NASA and the program

870
00:44:05,190 --> 00:44:07,414
were watching this core stage test.

871
00:44:07,414 --> 00:44:10,914
(rocket engines blasting)

872
00:44:12,000 --> 00:44:13,960
And we get to that first gimballing,

873
00:44:13,960 --> 00:44:17,631
it was the longest that I had ever held my breath.

874
00:44:17,631 --> 00:44:18,950
(rocket engines blasting)

875
00:44:18,950 --> 00:44:20,990
The only way I can explain that core stage test

876
00:44:20,990 --> 00:44:25,578
is the whole atmosphere was shaking like an earthquake.

877
00:44:25,578 --> 00:44:28,440
(rocket engines blasting)

878
00:44:28,440 --> 00:44:30,210
The thought goes through my mind still,

879
00:44:30,210 --> 00:44:31,910
how does that thing stay together?

880
00:44:33,292 --> 00:44:35,321
(rocket engines blasting)

881
00:44:35,321 --> 00:44:37,978
We were entering unchartered waters, if you will,

882
00:44:37,978 --> 00:44:40,300
to get to the end of the test and to run

883
00:44:40,300 --> 00:44:42,750
a full eight minutes and deplete

884
00:44:42,750 --> 00:44:44,485
both of the propellant tanks.

885
00:44:44,485 --> 00:44:46,130
(dramatic music)

886
00:44:46,130 --> 00:44:50,280
Being able to see Space Launch System come to life,

887
00:44:50,280 --> 00:44:53,510
do exactly what it was supposed to do and to perform

888
00:44:53,510 --> 00:44:56,840
and be able to deplete out the fuel system,

889
00:44:56,840 --> 00:44:57,860
that's a dream come true

890
00:44:57,860 --> 00:45:00,818
for any rocket propulsion engineer out there.

891
00:45:00,818 --> 00:45:05,818
(rocket engines blasting)
(dramatic music)

892
00:45:06,177 --> 00:45:07,910
It was extraordinary to accomplish.

893
00:45:07,910 --> 00:45:08,790
Chanel 16.

894
00:45:08,790 --> 00:45:11,653
There was a lot of emotion in the test control room.

895
00:45:12,640 --> 00:45:16,550
There was joy, there was high fives and hugs

896
00:45:16,550 --> 00:45:18,913
{\an8}and maybe a few tears that were shed.

897
00:45:20,990 --> 00:45:23,713
{\an8}It was absolutely a sigh of relief.

898
00:45:24,940 --> 00:45:27,820
{\an8}I saw these components as sheets of paper,

899
00:45:27,820 --> 00:45:29,880
and I actually saw them being built.

900
00:45:29,880 --> 00:45:34,760
Then I saw them all come together and work as a single unit.

901
00:45:34,760 --> 00:45:36,210
These are my babies, right.

902
00:45:36,210 --> 00:45:38,980
So when you go to a soccer game or football game

903
00:45:38,980 --> 00:45:41,410
for your child and they make a goal

904
00:45:41,410 --> 00:45:43,680
or they catch a ball, they hit a home run,

905
00:45:43,680 --> 00:45:46,020
you're gonna scream, right, "Yay. Good job."

906
00:45:46,020 --> 00:45:47,557
And so for me, I'm screaming for

907
00:45:47,557 --> 00:45:49,337
"Yay (indistinct), do your job.

908
00:45:49,337 --> 00:45:53,016
"Yay, prevalve, yay, feed line." (laughs)

909
00:45:53,016 --> 00:45:54,969
Safe and shutdown.

910
00:45:54,969 --> 00:45:57,900
(dramatic music)

911
00:45:57,900 --> 00:46:00,523
All personnel that fixes the page 656-

912
00:46:01,400 --> 00:46:04,790
We all took a few hours to celebrate that

913
00:46:04,790 --> 00:46:06,830
and then we were onto the next task,

914
00:46:06,830 --> 00:46:09,410
which was getting the stage loaded onto a barge

915
00:46:09,410 --> 00:46:11,501
and shipped to the Kennedy Space Center.

916
00:46:11,501 --> 00:46:14,334
(dramatic music)

917
00:46:18,600 --> 00:46:20,960
When the core stage arrived by barge,

918
00:46:20,960 --> 00:46:23,020
it did create a buzz, you know,

919
00:46:23,020 --> 00:46:25,030
that was a big day for us, right,

920
00:46:25,030 --> 00:46:26,630
because that was the very last piece

921
00:46:26,630 --> 00:46:27,830
of the puzzle we needed.

922
00:46:28,733 --> 00:46:31,240
(dramatic music)

923
00:46:31,240 --> 00:46:32,840
All the parts of the rocket are now here

924
00:46:32,840 --> 00:46:34,511
at Kennedy Space Center.

925
00:46:34,511 --> 00:46:37,344
(dramatic music)

926
00:46:38,470 --> 00:46:42,430
Now the next big step is we'll lift it and go up and over

927
00:46:42,430 --> 00:46:43,950
and into the High Bay 3

928
00:46:43,950 --> 00:46:46,063
and actually attach it to the boosters.

929
00:46:48,972 --> 00:46:49,805
(dramatic music)

930
00:46:49,805 --> 00:46:53,500
So now you have two boosters and a core stage.

931
00:46:53,500 --> 00:46:55,668
Then we just continue stacking.

932
00:46:55,668 --> 00:46:57,770
You start at the bottom and you just keep building blocks,

933
00:46:57,770 --> 00:46:59,832
you know, you just stack them and you keep going up.

934
00:46:59,832 --> 00:47:02,582
(dramatic music)

935
00:47:04,292 --> 00:47:05,125
(upbeat music)

936
00:47:05,125 --> 00:47:07,270
Among the last pieces to be stacked

937
00:47:07,270 --> 00:47:09,990
will be the crew and service vehicles.

938
00:47:09,990 --> 00:47:13,877
Our crew vehicle is the Orion Spacecraft.

939
00:47:13,877 --> 00:47:17,648
(light upbeat music)

940
00:47:17,648 --> 00:47:19,880
That Orion Capsule is a lot more than a capsule

941
00:47:19,880 --> 00:47:21,050
that goes to low-Earth orbit,

942
00:47:21,050 --> 00:47:23,330
it goes faster, has a stronger heat shield,

943
00:47:23,330 --> 00:47:26,630
it can handle the environment of deep space

944
00:47:26,630 --> 00:47:28,644
like the high energy neutrons much better.

945
00:47:28,644 --> 00:47:30,490
(light upbeat music)

946
00:47:30,490 --> 00:47:33,160
Space Launch Systems first uncrewed mission,

947
00:47:33,160 --> 00:47:37,100
Artemis 1 would be a momentous flight for the rocket,

948
00:47:37,100 --> 00:47:40,080
but more importantly a critical validation

949
00:47:40,080 --> 00:47:42,780
of the Orion vehicle's safety.

950
00:47:42,780 --> 00:47:44,620
The main thing they want is a successful

951
00:47:44,620 --> 00:47:48,460
loop around the moon, come back and then test that re-entry.

952
00:47:48,460 --> 00:47:51,860
And that reentry should be capable of bringing them back

953
00:47:51,860 --> 00:47:55,070
from lunar orbit at about 25,000 miles an hour.

954
00:47:55,070 --> 00:47:58,350
So it'll be a high performance reentry shield

955
00:47:58,350 --> 00:47:59,482
that's for sure.

956
00:47:59,482 --> 00:48:01,430
(pondering music)

957
00:48:01,430 --> 00:48:05,704
That was one of our prime objectives of developing SLS.

958
00:48:05,704 --> 00:48:07,790
(pondering music)

959
00:48:07,790 --> 00:48:11,290
And in Artemis we will be carrying Orion and the crew

960
00:48:12,450 --> 00:48:13,283
to the moon.

961
00:48:16,040 --> 00:48:18,370
The Artemis project is something that encompasses,

962
00:48:18,370 --> 00:48:21,270
you know, nearly everything we're doing at NASA right now.

963
00:48:23,030 --> 00:48:26,210
In my team, we do a lot of the propulsion testing

964
00:48:26,210 --> 00:48:29,410
for the technologies that Artemis is going to rely on

965
00:48:29,410 --> 00:48:31,700
to get back to the moon and to go beyond.

966
00:48:31,700 --> 00:48:33,370
(pondering music)

967
00:48:33,370 --> 00:48:34,930
I mean, sometimes it can be overwhelming

968
00:48:34,930 --> 00:48:37,170
when you think about everything in the daisy chain

969
00:48:37,170 --> 00:48:40,290
that has to go right to be successful.

970
00:48:40,290 --> 00:48:42,790
But you know, if it was easy,

971
00:48:42,790 --> 00:48:44,803
everybody would be doing it, right.

972
00:48:46,530 --> 00:48:49,440
It's not meant to just, you know, take a return visit

973
00:48:49,440 --> 00:48:50,700
back to the moon.

974
00:48:50,700 --> 00:48:54,550
We will be able to create a presence on the moon,

975
00:48:54,550 --> 00:48:57,720
a lunar outpost that we'll be able to facilitate

976
00:48:57,720 --> 00:49:00,240
multiple visits to the moon and then venture

977
00:49:00,240 --> 00:49:03,333
onto deep space destinations, including Mars.

978
00:49:04,817 --> 00:49:08,210
(dramatic music)

979
00:49:08,210 --> 00:49:09,950
We know what's at stake,

980
00:49:09,950 --> 00:49:12,800
not just all the work that's been put forth for everyone,

981
00:49:13,670 --> 00:49:15,867
it's also the lives of astronauts.

982
00:49:15,867 --> 00:49:17,950
(dramatic music)

983
00:49:17,950 --> 00:49:20,030
We need to make sure that we're a program

984
00:49:20,030 --> 00:49:22,410
that can sustain itself, that meets that mission

985
00:49:22,410 --> 00:49:24,492
to take us all the way to Mars.

986
00:49:24,492 --> 00:49:27,220
(dramatic music)

987
00:49:27,220 --> 00:49:30,270
For me, these hard missions, these missions that we do

988
00:49:30,270 --> 00:49:35,035
because they are hard, they measure the very best of us.

989
00:49:35,035 --> 00:49:38,500
(dramatic music)

990
00:49:38,500 --> 00:49:41,080
They combine our efforts across nations

991
00:49:42,320 --> 00:49:44,915
and across people groups.

992
00:49:44,915 --> 00:49:46,670
(futuristic music)

993
00:49:46,670 --> 00:49:48,091
They make us better.

994
00:49:48,091 --> 00:49:50,841
(dramatic music)

995
00:50:00,459 --> 00:50:03,459
(light outro music)

996
00:50:34,554 --> 00:50:37,050
(light outro music)

