The video takes a detailed and captivating look at the incredible Saturn V rocket, a monumental human achievement in space exploration. The host introduces viewers to Luke Talley, an esteemed engineer from the Apollo program who worked on the rocket’s instrument unit. Through Talley’s firsthand knowledge and experience, viewers learn about the intricate workings of the Saturn V, including its various stages and the technology used to guide it to the moon.

This video is especially compelling as it provides a blend of historical context, personal stories, and technical expertise. Viewers gain a unique perspective on the challenges and triumphs of the Apollo missions and in-depth insights from a person closely involved in the engineering feats of the program. The blend of personal anecdote and technical description offers an engaging narrative that enriches one's appreciation of space exploration accomplishments.

Main takeaways from the video:

Please remember to turn on the CC button to view the subtitles.

Key Vocabularies and Common Phrases:

1. astounding [əˈstaʊndɪŋ] - (adjective) - Causing amazement or wonder, quite remarkable. - Synonyms: (amazing, astonishing, startling)

One thing you'll notice is Luke's ability to recall facts and numbers is astounding because he actually lived this.

2. kerosene [ˈkerəsiːn] - (noun) - A flammable hydrocarbon liquid commonly used as a fuel. - Synonyms: (paraffin, jet fuel, fossil fuel)

The fuel is kerosene and liquid oxygen, of course, the oxidizer.

3. gimbaled [ˈɡɪmbəld] - (adjective) - Mounted on a pivot or free-moving support, allowing rotation. - Synonyms: (pivoted, swivelled, oscillated)

The four outer engines are gimbaled.

4. actuators [ˈæktʃuˌeɪtərz] - (noun) - A mechanism that puts something into automatic action or movement. - Synonyms: (drives, controllers, motors)

They have actuators? Will you show me? Can you see this pointer? Yeah, a little bit

5. pyro detonator [ˈpaɪroʊ ˈdɛtəˌneɪtər] - (noun) - A device used to initiate a powerful explosive reaction. - Synonyms: (explosive device, igniter, detonator)

Every single component of the rocket that had some type of pyro detonator, a rocket that had to cut on.

6. combustion [kəmˈbʌstʃən] - (noun) - The process of burning something, usually a chemical reaction involving rapid combination with oxygen to produce heat and light. - Synonyms: (ignition, burning, incineration)

Several injector designs, such as this lox dispersion injector, have been tested in an effort to increase combustion stability margins.

7. vibration [vaɪˈbreɪʃən] - (noun) - An oscillation or repetitive motion, often creating shaking or trembling. - Synonyms: (tremor, oscillation, quiver)

Except in that high vibration period.

8. telemetry [təˈlemətri] - (noun) - The process of recording and transmitting the readings of an instrument. - Synonyms: (data transmission, remote measurement, monitoring)

The telemetry systems and so forth, the environmental control system.

9. hypergolic [ˌhaɪpərˈɡɑlɪk] - (adjective) - Describing a type of propellant or fuel that ignites spontaneously upon contact with an oxidizer. - Synonyms: (self-igniting, non-explosive, reactive)

These are hypergolic, you know, nitrogen tetroxide, whatever that other stuff, hydrazine.

10. orbital plane [ˈɔːrbɪtl pleɪn] - (noun) - The flat, disc-like expanse along which an astronomical body orbits in space. - Synonyms: (galactic plane, trajectory path, orbital path)

All right? So what you do is you wind, you launch and you wind up in an orbit about the earth, but the orbit plane is in a different plane from the plane of the moon that's also orbiting the earth.

I Asked An Actual Apollo Engineer to Explain the Saturn 5 Rocket - Smarter Every Day 280

The Saturn V rocket is one of the most amazing vehicles ever created by humans. And if you could have one person explain the Saturn V to you, who would it be? Today on smarter every day were in the middle of a series about going back to the moon. We looked at how the Apollo astronauts trained to go back to the moon on something called the lunar Lander test vehicle. We even spoke to one of the original engineers over that program. We also looked at one of nasa's early ventures into autonomously landing on the moon, something called the Mighty Eagle.

We also took our first look at the Saturn V. We got to meet an engineer named Luke Talley. He was one of the original IBM engineers over what's called the instrument unit. This is the large computer shaped like a ring up near the top of the rocket that steered the rocket towards the moon. Now it's time to go deeper and understand the entire Saturn V rocket. Wernher von Braun said, as the IU goes, so goes Saturn. That right there is none other than Luke Talley. So there is no better person to explain to us how the Saturn V works than Luke. He understands how all three phases of this rocket works, because the IU has to control the entire rocket.

Today we're going to talk to Luke Talley in great detail. Detail. But before we do that, I want to tell you a little bit more about the person that Luke Talley is, because that will influence how you feel when you're receiving this information. November 10, 1944. A young sailor from Alabama is killed in the Pacific theater in World War ii. And this young sailor had a three-year-old boy and a wife back home in Alabama. This little boy turned out to be extremely curious, and like most little boys of the time, he loved making crystal radios and things like that. But he couldn't afford kits like this because they were kind of bootstrapping everything.

Didn't have a lot of money, so a lot of people in the community helped him put together things like this, just different parts. You could make your own crystal radios and stuff like that. And that's what he did. And it became clear that this young boy had an aptitude for electronics, which is why Luke was able to use his dad's GI Bill, because his dad couldn't use it. And Luke went to the University of Alabama to study electrical engineering. I want to show you this picture.

This is Luke and his wife Kitty. This is Luke's favorite picture in the entire world. This is them all decked up on the. And she's sitting there on the hood of the 57 Chevy. This is a really cool picture, because Luke and Kitty got married shortly after this photo, and he studied electrical engineering at the University of Alabama, and that's what started his career. After that, he went to IBM, where Luke quite literally became an award-winning engineer on the Apollo program.

This is a plaque that was used at IBM as part of the instrument unit team. You can see that it's signed by Alan Shepard, hailing Luke as a pretty important person. This is part of the manned space flight awareness coordination effort there, where they would make the employees that were working on the hardware know more about what was going on. Luke solved a really big problem. There was a problem on one of the early Apollo missions where a coax melted because it got hit by the sun on its way to the moon.

And Luke and his fellow engineer here, they solved this problem, and Luke was awarded an award. This is the result of that. He got to go see the launch of Apollo 13. And you can see this right here is where he was given that award. They were talking about all the things he did and the fact that he was invited to attend the launch of Apollo 13 at Cape Kennedy on April 11. This book, which is one of Luke's most prized possessions, I can't believe he let me borrow it, has all kinds of things.

You can see pictures of Luke and his wife attending the launch, all sorts of stuff like this. They have different meet and greets with astronauts at that launch. So you can see Luke Talley is not just a normal engineer. He is an award-winning Apollo engineer. I thought this was cool. You could see the name tags. They're really, really interesting.

And perhaps one of my favorite photos is this one right here. You can see Luke and his young bride kitty. You can see them at the launch pad for Apollo 13. What I think is so amazing here, as you can see on the side, if you look really, really close, it says April 1970. That's amazing. So, as you can see, Luke Talley is the perfect person to teach us about the Saturn V. He's seen one launch, and what's even more impressive to me is that the instrument unit that he worked on had to touch every single component of the rocket that had some type of pyro detonator, a rocket that had to cut on.

They had to program everything, so they had to know exactly when it needed to fire. So for those reasons, I'm excited to introduce you once again to Luke Talley. Who is going to teach us about the Saturn v. Let's go get smarter every day. We're going to meet Luke here at the US Space and Rocket center early one morning before the museum opened.

And one thing you'll notice is Luke's ability to recall facts and numbers is astounding because he actually lived this. He moves pretty fast, so try to keep up. But what we're going to do is we're going to start at the first stage, then move to the second stage, then the third stage, and then we're going to talk about the launch escape system along the way. We'll talk about some other things, but here we go. Let's learn about the Saturn V from Luke Talley. I call this the. This is the mouth dropping entrance of the Saturn hall. And you come in here and you see these, each of these about 12ft in diameter.

Each of these engines now produce one and a half million pounds of thrust each. The four outer engines are gimbaled. That is, they can move, they control by the computer up in the instrument unit, which is on top of the third stage during the flight. The first stage will go through the speed of sound at about 60 seconds. Shortly after that, you get the maximum aerodynamic pressure on this vehicle and it is like two giant hands have it, shaking it for all it's worth. Each of the engines can move anywhere in a five-degree circle.

As we go through the speed of sound and we get maximum aerodynamic pressure, we would see them move about one and a half degrees. That's the most we ever saw move most of the time, except in that high vibration period. They would move it maybe a half a degree. And that was actually pointing the rocket? Yes. And that steers the rocket. So you move these four outer engines as you need to, to steer the rocket.

When you move the engine, you not only move the rocket, but you cause it to flex. These engines are so powerful that there are points in the flight where if you move this engine too quick, you can break it in two. Break the rocket into, not the engine. Oh, wow. And what are these engines? What are they called? These are called f one. I have no idea why it's f one. That's just the number.

Okay. The thing that to me is just incredible is each one of these engines. Now, the fuel is kerosene and liquid oxygen, of course, the oxidizer, this thing burns a ton of kerosene and two tons of liquid oxygen every second, each engine. Because when you say, man, this does a ton of whatever, that's right. You're doing hyperbole, but you're literally saying a ton of kerosene. That's right. I per engine.

So these, these five engines are burning 15 tons of propellant every second. So the mass of this thing changes very rapidly, and that affects these bending modes. So we had to measure that kind of stuff and program again into the computer system so that we knew not to. So you're saying each of these engines can move. Each of the four outer engines can move. The center engine's fixed. It doesn't move. Well, how do they move? Do they have.

They have actuators? Will you show me? Can you see this pointer? Yeah, a little bit. Okay, so that thing right there is an actuator. Engine has an actuator. There's an actuator here, and then there's another one up on the other side of it up there. So two actuators per engine.

The actuator is a hydraulic actuator servo mechanism under control of the computer in the instrument unit, and they're using the kerosene as their hydraulic fluid. There's plenty of pressure in the tank, so I don't need a pump. So I'm saving weight and complexity and so forth. And they look at it and you say, you sure, we saved any complexity? But that's true. Oh, so there's like a lot of aerodynamic or aerospace systems. Have a hydraulic fluid. Oh, you have a hydraulic fluid. Well, the upper stages.

Upper stages have to have the hydraulic fluid, but this thing, we just use the kerosene. Interesting. And that saves a whole set of piping. Whole more set of piping. Complexity affects your reliability. Number one concern is reliability in this thing. You want to have it as perfect as you can because there's, you know, there's 5 million parts or something like that in this thing. So every part, if it's 0.9 times, I got 5 million of them, and that ain't real good.

So I need 0.999, you know, so I gotta have 99.999 something percent chance of making the mission. In order for all this stuff to work, that has to. So that's one of the main issues. Now, the engine itself, as you look at the engine, can you look up there? I can barely see your laser, but you're pointing in this area right here. Okay, so we have the thrust chamber, and then we have a nozzle extension on the back. But the interesting part of this engine is all this mounted up above the thrust chamber.

Okay. This is a jet engine to drive the pumps, to get three tons of propellant through that engine every second. So this is a jet turbine in here. And this jet turbine is about a 50-odd thousand horsepower turbine. The helicopters that fly around Huntsville, probably five to 7000 hp engine. So this is a monster turbine. Probably. One of the more interesting points of it is the thrust chamber itself.

The throat temperature is 5900 degrees. That melts stuff that will melt any of these materials. So what they do is if you can see this, it has fine tubes running down this thrust chamber region here. The kerosene, before it's burned, is actually routed down these tubes. Okay. Comes down a set of tubes, goes back up another set of tubes, then in the engine to burn it. And the flow of that in the wall is how you're cooling that engine to keep it from melting.

Now the oxygen was, was liquid oxygen, right? Was the kerosene super cold or. No, it's just plain old liquid kerosene. Okay. You throw all that down in here into the combustion chamber. Yep. And what does that look like, that mixer plate there? The injector plate is just a large diameter plate, has about 6000 holes in it. Some of the holes are squirting kerosene, some of the holes are squirting liquid ox. Do we have something here in the museum that shows it? Yeah. So we can see that. Yep.

Interesting. And so you said the four on the outside would gimbal. That's right. But the one in the middle does not. So how do you, with the computer, how would you know which ones to control? Would you, could you? Well, your guys, you have a guidance platform in the instrument unit and it's telling you where you are and you have a stored profile of where you want to be. So 25 times a second he's reading the guidance platform and calculating or part of the calculation for where am I versus where should I be.

Based on that, he determines which engines need to be gimmeled in order to steer you in the right direction. Do I need pitch? Do I need yaw? Do I need roll? Do I need all the above? And all of that's done in the. And it's a closed loop system. Yeah. That's amazing. The thrust chamber up there where we're talking about the little tubes, that's all made out of a metal called inconel. Nickel, cobalt, chromium, very corrosion resistant.

This sucker is burning two tons of oxygen every second. So if it's a piece of iron, it would melt, it would rust in a heartbeat. So they had inconel blankets. The engines, they had blankets on the engine. They had blankets on the base. The problem you have with this thing, once you get up a little out of the atmosphere, that center engine gets extremely hot from all the heat coming off of these. So you're trying to keep as much heat as you can away from that center engine.

Oh, interesting. Because you're kind of in a low-pressure zone back there. Oh, yeah. Yeah. Because you're moving forward and you got this little pocket. That's right. Interesting. Everything is blanketed with an insulating blanket to try to keep all the heat in the engines instead of dumping it over on that poor center engine. Interesting. I didn't know that. That's amazing.

We say in south Alabama, he's hotter than a two-dollar pistol. I like that song too. That's amazing. So in here, as you look at this thing, you see there are parts on here that are yellow. Anything in here that's yellow is ground handling equipment. So you see those plates are there and that's so this thing won't sag as it's laying on its side. So once you get it up, stand on the pad, you would remove the yellow pieces. We'll see a lot more of that on the forward section. And that's the original design for the hardware.

Yeah, yeah. Okay. All right, following you. Okay, so the first stage will burn two and a half minutes. Takes them up to about 40 miles high and 5000 miles an hour. Now, at that altitude, you're pretty high, you know, 40 miles up. Well, he's still climbing as he's at separation. So when things separate, you think each of these engines back here is nine tons. So we got 45 tons of engines. They attach to a cross member of aluminum. That's another about 20 tons.

So we got 60, 70 tons of stuff. So you would think the rocket is climbing. He would do this and fall, but he's going 5000 miles an hour. When it separates from the second stage, it does sort of tilt down. But this thing will go almost 70 miles high before it finally starts coming down. Falling from 70 miles. When it hits the Atlantic, it pieces just go everywhere. Kablooey. Yeah, kablooey.

To be clear, the reason you separate the rocket is you've got all this extra mass trying to get rid of everything you've used. Once you're out of all that fuel, sitting on the padded, we're about six and a half million pounds. The first stage is like over 4 million pounds of that. The first stage is a big chunk, but it gets you up and gets you up through the atmosphere and on your way up to 5000 miles an hour. So as you walk up beneath the thing, you'll see there's smooth sections and corrugated sections.

The smooth section directly above where I'm standing right now has the USA on it is a fuel tank. Okay, so that's where the kerosene is. This thing is made out of aluminum plate. Inch, inch to inch and three-quarter thickness. They form a flat plate. They mill the inner surface for strength and some slosh baffling and then they put this thing in a giant press and bend it. Well, this plate is about, is one-third of the circumference. Then they take these plates, stand them up, and they have this automated welder. As I recall, there was something like, something like 20 to 30 passes to weld this inch and a half inch quarter thick aluminum plate. I remember some of the mechanical guys talking about it.

They would set the thing up. We would put up these, what we call test coupon, just a, you know, a piece of aluminum to check out the well to make sure it's okay. So they make the wells, then they take this thing, slice it up, put it on the microscope. And they said you would be hard pressed in most cases to tell the virgin aluminum from the weld. It was very, very precise. So they were super skilled craftsmen? Yes, yes.

The forces from the engines are transmitted out through this structure we were talking about. And all the forces are transmitted upward through the skin. There's no internal beams or anything like that. So all your forces are going through the skin. Well, the tank now has to withstand the upward force plus the pressure in the tank, called a hoop stress. Yes. Okay, so the tank area is, has to withstand more forces than do the inner tank areas. So the inner tank areas are made with this corrugated material.

So I can use a lot lighter weight material because I'm only having to withstand upward force. I don't have any inside pressure. Oh. So. Well, correct me if I'm wrong on this, Luke. So right there, I'm looking at the corrugated stuff, right. It has a bigger cross section so that it can withstand more axial force. Well, it's just. No, it's just, it's just corrugated to give it more strength. So it's not going to buckle. Right.

So are there tanks inside? Like, am I looking. So this is a model? I don't know if this is a correct model. Yeah, this is a pretty good little model. If you look, the fuel tank is the lower section down here. And if you look inside the tank, you can see that the liquid oxygen lines actually run through the fuel tank. Those things are about 18 inches in diameter, and if you had to bring them out around the tank, you would mess up your streamlining on your rocket, on your surface.

So they're actually going through it. Now the problem you have here is liquid oxygen would freeze the kerosene. So the piping that's going through there is kind of like a big thermos bottle. Okay, so you're saying like this is the, this is the liquid oxygen, that's the oxygen tank. So the oxygen sat above the kerosene and these pipes that go in between the two, you've got these big pipes that go. They sure do. How many are there? Is there one for each engine? Just a direct line? Yep.

Okay. And so you want to make sure that you don't have frozen kerosene around that. So is double-walled or how do they do it? Yeah, it has an inner wall, outer wall, and then it has a low-pressure gas in between, just like a thermos bottle, really. And the purpose of the low-pressure gas is to insulation. Wow. Okay. So volumetrically, how does the chemistry work? Do you have more fuel or more oxygen? Oxygen. More oxygen, yeah.

So how does that. Well, you look up here, you're about a two to one. Where does the oxygen start? The oxygen tank is in the smooth section up top. Up here. Okay. One right above us was the fuel tank. This now is the oxygen tank. You can see there's about a two-to-one. Two to one. Okay. Wow.

So, and they density is about the same, is it? Okay, hydrogen, I mean, oxygen is like nine pounds per gallon. kerosene like seven, I think. Really? So we're still under stage one? We're still on the first stage. We were talking about the injector plate. Down in the throat of the engine is this injector plate got something like 5000 holes or something like that.

And some of the holes are spring kerosene, some are spraying liquid oxygen and you have these baffles. When this engine was first made, the air force started development of this engine. Early on. They thought that nuclear weapons were going to be much heavier than they turned out to be. So they thought they were going to need a heavy lift rocket. They thought they were going to put manned orbiting laboratories, spy in the sky type things. And ultimately the technology got ahead of them.

So this engine was transferred to NASA to follow to resolve the final issues and use it on the Saturn. Originally, it did not have the baffles. The problem is this stuff spraying in here starts a circular rotating motion. So this gas starts circulating in this giant, like we're talking about stuff swirling around maybe 2000 revolutions per minute. I mean, it's really moving in there. Problem you get with that is these injectors, sometimes they mix, sometimes they don't mix well. So you wind up, you can get an engine that I'm getting too much oxygen in an area and not enough kerosene, it turns into a settling torch and cuts the end off of the bell, really?

And then the other problem you have is if I get too much kerosene and not enough oxygen in this thing, it starts like a car that's running rough on the road. So now it starts, this terrible vibration will shake it to pieces. So the baffles break that swirling motion up into much smaller areas that then don't have such a major effect on it once they put the baffles in. And this is only happening in the first few inches of the injector. So first few inches into the engine, off of the injector. So these baffles were enough to solve the problem. Several injector designs, such as this lox dispersion injector, have been tested in an effort to increase combustion stability margins.

Other designs tested include the baffled divergent ring injector, low fuel delta P injector, 21 compartment baffled injector, and the divergent ring injector. So basically what they're doing is they're controlling a very huge turbulence problem. That's right. They're cutting it into smaller chunks and then that way you can get more complete mixing in these sections. That's right, yep.

Are these the pipes you were talking about here? Yeah. So these are, these are the tubes, the inconel tubes, where you're pumping the coolant. Now this big baffle around this thing, we take the jet turbine, there's a nozzle extension on the engine, which is not on this one. Lying on its side another six 7ft of engine out here. That's a nozzle extension. Well, it's made out of high-strength stainless and what they actually do is they take the turbine exhaust.

The turbine now is running a fuel-rich mixture, so its exhaust temperature is only about 1200 degrees. So by capturing that exhaust and routing it around here and then injecting it into the walls of this nozzle extension and then having little openings around the interior of the extension, the flow of that exhaust in the walls is how you're cooling the nozzle extension. Kind of hard to think of cooling with 800 degrees, but it's better than 5000. Wow.

And then you allow the exhaust to be injected into the nozzle, and that way, your extra thrust you're getting out of that is put in the direction you're going. That thing will produce about 18 to 20,000 pounds of thrust. So if you squirt it out to the side, you'd forever be correcting with another. Just the cooling section is 18,000 pounds. Just the. Well, the exhaust from the. Oh, I see.

Turbine. So you have to control where the coolant goes directed into the thrust chamber so it's going in the direction you're going. Okay, Luke, you're absolutely right. We could do this forever, couldn't we? Yes. Right. I don't know how you're gonna cut this? Oh, man. That's quite the reveal for stage two. We'll hustle.

Okay, now we get to the top of this stage we were talking about ground handling equipment. You see this big yellow structure on the top of it? This is how you lift this thing off of the transporter and pick it up and put it on the launch pad. Then you would remove this yellow structure up here.

And then there's a piece missing that would go from the base of the stage out about where I'm standing. I think it's twelve or 15ft, something like that. So you and your team, whoever, whoever controlled the firing and the timing sequences and things like that, so we've lit off the engines, we've burned all of our fuel, and it comes time to do separation. So you have to shut the.

So you have to shut those engines down. Miko. Main engine cutoff. That's right. And then there are four fins on the base. There's a fairing that flares out so that your engine, when you can gimbal it without the atmosphere streaking by and holding you, keeping you from gimbal. All right? And then in that fairing, there's a fin, alright?

There's four of them around it. Well, at the base of that fin pointing in this direction, they're two big solid rocket motors. So there's eight of them around that thing. So this thing is connected to this interstage with a set of. With a piece of ordinance. Okay, so you computer says, all right, time to shut it down. Main engine cutoff fires this ordinance. This ordinance now separates.

The stages are strapped together with tension straps. Around the interior of those straps is the ordinance. Computer fires the ordinance severs these same time fires those retro rockets to slow this thing down, doesn't back it up, just slows it a little bit. This piece that's missing up here, the interstage, there are eight more solid rocket motors around it and they're fired at the same time to put thrust on the upper, on the second stage to keep the propellant seated in the tank.

So I can get these engines started because of slosh. That's right. You gotta get that stuff down in the tank. Otherwise when you shut off, it just kind of wants to float forward. Okay, so you have to a little bit of thrust to pull that stuff back and get these engines going. Once you get these engines going, then you jettison this interstage and that's to get rid of excess weight. So there's a lot more going on in stage separation.

Okay, so check me here. So, engines cut off and then we blow the tension straps here. And then we have those retro rockets on the fins. Fire those to slow this down. And then we have a kick right here. Then we have these. These are called ullage rockets. Oh, okay. So we have a little bit forward.

A little bit. Yeah, a little kick in the pants. Seatma tanks, fuel and propellant tanks. And then start these engines. Now, these engines, first stage, one and a half million pounds of thrust. F one s. These are j two engines. The fuel here is liquid hydrogen. So hydrogen gives you a lot more efficiency.

But, boy, hydrogen's really tough to mess with. 426 below zero. So everything in a whole different world now from messing with a bottle of kerosene versus this stuff. Okay. But more efficient. So each of these engines, now, the first stage, remember we were burning three tons of propellant every second to produce one and a half million pounds of thrust. These are burning about 600 pounds a second to produce 230,000 pounds of thrust.

So this, these five engines equal about one of those first stage engines. I see. But you have less mass that you're hauling around. That's right. And so you don't have to accelerate all that saying I'm carrying hydrogen, which is pretty light. Okay. Hydrogen density.

Remember we said liquid oxygen is nine pounds per gallon. Liquid hydrogen is seven tenths of a pound per gallon. Oh, wow. Okay. Now the difference there means that these pumps on these poor little engines, they have to work really hard. The pumps that we were spinning, the turbine that is spinning the pumps on the first stage engine at about 5000 revolutions per minute. Okay. The oxygen, I believe the oxygen pump on this one is about 6000, 8000 revolutions per second per minute.

And the hydrogen is 37,000 revolutions per minute. Oh, I see. They're working hard because hydrogen is low density. It's got to work very hard to pump a bunch of that. So volumetrically, you're having to pump a lot faster because you have less mass, but you still need the same amount of. Well, you need a lot of mass in order to make the chemistry work. Yeah, you got to get some oomph out of it. That's technical talk. That's amazing.

So where are again? So they're on each engine? Each engine has its own. So we have five engines here. Four outer engines are gimbal just like the first stage. These, I think first stage could move five degrees. I believe these would operate closer to ten degrees.

And you're controlling these with your computer screen? These are all still under control of the instrument unit? Everything's under control. Everything we've talked about so far is under control of the instrument unit. Well, how do you connect the computer from. So that means the instrument unit, which is over there. It's on the top of the third stage. It's way up there at the top of the third stage. How do you connect the computer? You got cables going down, all the way down.

Where would they be? They would be in going between the stages. And you won't see them on here. Okay. They're on the interstages. They have disconnects. Okay. And then they have a backup guillotine crack. Make sure that sucker's cut free.

Really, I don't want this thing hanging on a cable back here. So it's a blade, explosive blade. So the stages are all connected through their independent lines from the instrument unit. Now, there are not many lines there, you know, probably 20 or 30, not too many. Yeah. That's amazing. And so this engine, what was it called? J two. The j two engine.

Yep. J two. That'd be on the second stage and the third stage. So a lot of people spent their entire lives just working on this engine. Oh, yeah. A lot of people spent their entire lives working on one part of that engine. Really? It's kind of the way it goes.

And then here you come along, and you get to control everything. That's right, yeah. Okay. Well, above us is the s two stage. All right. Now, the s two, we got a little bit of corrugated, but most of it is smooth. Okay. All right, so in the first stage, remember, we had the hydrogen, we had the kerosene tank, and then we had the liquid oxygen tank.

And they're two totally separate tanks here. We have a deal where there's a common bulkhead between the two tanks that saves a tremendous amount of length, which saves a tremendous amount of weight. I don't have a hemispherical tank here. And then another one up here. Actually, I've got one surface. And that surface serves the oxygen tank below and the hydrogen tank above.

But they share one of the bulkheads of the tank. They share. Okay, now, this stage you see above us up here, it has sort of a funny-looking surface to it. This was a phenolic honeycomb grid, and then it was filled with foam. The hydrogen tank is so. Hydrogen is so cold. 426 below zero. You really have to insulate it. And you have to insulate it very, very good.

The problem you run into is if you don't insulate that tank, the boil off from it will be so great that you can't fill the tank. So you got to insulate it to fill it. Number one. Plus, you got to insulate to make sure it lasts any time. So the second stage is insulated on the outside. This was used on some of the early flights. This phenolic deal. Later on, as my understanding is, they went to, like, big styrofoam blocks, just glued to the outside. It worked a lot better.

Upper stage. Now, the upper stage will last. First stage, we were burning two minutes, two and a half minutes. This one's going to burn about six minutes. So not long into the flight, these two stages are gone. But the third stage, now he's going to go in orbit and it's going to be a number of hours before we're through with it. It's actually insulated on the inside of the tank. Really? Okay.

Now, when you come to the end of the second stage, beginning of the third, we've got another interstage, and of course, it's missing here. So there's a tapered section that goes. The first two stages are 33 ft. in diameter. The third stage and the instrument unit are 22 ft. in diameter. And the spacecraft is 11 ft. in diameter.

They knew there were going to be a lot of us Alabama guys working on it. So, 33, 20, 211, and we're keeping it simple. You don't have to put that in. Somebody did make a decision, though, didn't they? Okay, so now when we get to the third stage, we've only got one engine. Okay, well, before the first two stages, we've got four outer engines and we can gimbal those and we can make the rocket pitch. We can make it yaw and we can make it roll.

With one engine, I can pitch and I can yaw, but I can't make it roll. Interesting. So the two black pods, there's one up here on the upper right, there's one on the left. Probably can't see it. There's a set of thrusters in there to give us roll control while the engine's burning.

What's that called? Is that called the reaction? This is called the auxiliary propulsion system. Ap's. These are hypergolic, you know, nitrogen tetroxide, whatever that other stuff, hydrazine. Hydrazine. When they squirt it into the chamber, it immediately burns. You don't have to have an igniter. Okay?

So during the boost phase, they have the AP's gives you the roll control. Now, this will go into orbit and will coast. And while we're coasting, there are roll pitch annual thrusters in there to control it. And you were controlling those and it's all under control. Computer instrument. Right.

First stage, shut down at about 40 miles high. And then it went on up higher and then fell into the ocean. Wound up about 450 miles from the cape. In the atlantic, they put out maritime warnings. You don't want that thing to fall on your boat while you're out there fishing.

The second stage, now he shuts down. The first stage was still climbing. This one. Now he's up to about 115 miles high, traveling 15,500 miles an hour. He's going to do a nose dive into the atmosphere. Going into the atmosphere, probably begins to break up at altitude. Doesn't burn up, just breaks up in pieces in the neighborhood of 2000 miles, 2500 miles from the cape, something like that, in the Atlantic.

Okay, now the third stage is going to burn for about two minutes. Okay, now he's going to take them up, not much higher, 117 miles higher, probably 17,500 miles an hour puts them in orbit. Now the problem we have here, or the situation, we're going to the moon, but we launched from the cape. You can only launch in certain directions from the cape. All right? So what you do is you wind, you launch and you wind up in an orbit about the earth, but the orbit plane is in a different plane from the plane of the moon that's also orbiting the earth.

All right? So we go into orbit, we shut this thing down. Usually coasts an orbit and a half. We could have coasted as much as 6 hours before we ran out. Okay, usually only orbit in half hour and a half or so, 2 hours. And what we do is when our orbit, we come around in our orbit and it intersects the plane of the moon's orbitz, we restart this engine again. So this one burns twice.

Now he will burn for about six minutes and will take them out of the moon's plane. I mean, out of his orbit plane and into the moon's orbit plane and up to 24,500 miles an hour. Now they're on their way to the moon. After that, the crew's got to get separated and do all their magic. So we'll talk a little bit about that if you want to.

Let's do it. Where do you get rid of the third stage? I mean, does it go to the moon with you? Oh, we'll get back to that one. That's a good one. Okay, so we won't spend much time on the spacecraft. We'll just say, here's where it is. Yeah, we'll just. We won't talk much about the little thing that went to the moon, like the actual land part, if you want to know about that.

Go to Johnson Space center. Here's probably the best little thing you can show is this model here shows the third stage, the instrument unit, and the lunar module is inside what's called the spacecraft lunar module adapter, the SLA. The SLA. And then the service module atop that. And atop that is the command module. And this is where the three astronauts are located.

Now, this launch escape system up here on top of it, if we had to abort during the first stage burn, if we lost two engines, or the rates got too high if the rates get too high on that first stage, you can break this thing in two also. So that is an emergency. Get them off of there right now. So there's an emergency detection system, hardware in the instrument unit, we don't need the computer. We don't need any of this. It's all hardwired.

It's triple redundant and everything. So if I lost two engines on that first stage, that system would automatically fire a rocket motor that's in that launch escape tower up there. That thing would pull just the command module with the crew. And, you know, the crew members are inside, the astronauts are inside there. So this thing now would pull them wherever the abort occurred, would take them 30 to 40,000 ft. higher, then it would jettison and they would come down on their parachutes. And so I'm looking at it only in first stage burn.

I'm looking at it right there. So I can see the nozzles on the backside. So that's a rocket, a solid rocket motor. Yeah. And those nozzles are pointed out. That's right. And that's to not burn the top with the gumdrop. Don't bell, don't melt the spacecraft. Now, the spacecraft during that point, as they're going up, in case you were to have an abort, that launch escape system actually has a cover that is actually over the top of the spacecraft. Until they jettison this during second stage burn, they can't hardly see anything.

There's a little window down at the side they can see out, but the main one, they can't. It's covered. And that's in case we had to fire that thing. We wouldn't damage the spacecraft. Yeah. Interesting. And when the launch escape tower separates, it pulls that conical section with it as part of the. So when does that fire?

I mean, you got to during second stage. Just after the second stage burn starts. Okay, so it's afterwards. So you jettison it while you're firing the second stage? Yes. Really? Yeah. Okay. I didn't realize it has a little motor up at the front of it that will. Will pull it away and pitch it up out of the flight path.

So there's a little motor on top of that? Yeah, there's a couple of little extra auxiliary motors inside that thing. Is it a pretty dumb rocket up there? It's solid, right? Yeah, it's solid. That thing has as much thrust as a Redstone rocket. Just doesn't burn as long. It'll snatch them away there real quick. They will pull some G's. They'll probably be sore if that ever happens.

Luckily, we never had that happen. That's amazing. I did not realize that you jettisoned that. Is that the word, jettison? I didn't realize you jettisoned that while the second stage was burning. Yeah, just after the second stage gets up burning, then you get rid of it. Now, the instrument unit, we talked about it.

This is where it's located, on top of the third stage. Okay. Now, when we get to this point, we will just. The lunar module is inside the tapered section up here. We've jettisoned that launch escape tower, so it's no longer there. The command module and the service module are going to stay together until just before they re enter the Earth's atmosphere, coming home.

So at this point now they're heading toward the moon, where, you know, we're probably six or 800 miles above the earth, not very far yet. Still got about three days to get to the moon. So the crew now the command modules, service modules, together, they will separate from this, the slaw, the spacecraft, lunar module adapter. They will separate and move away from the space, from the rocket, and then they will turn around. Okay, as they're turning around, we'll jettison four panels on this slaw here, which, as part of the instrument unit control stuff.

Again, the center command will jettison these four panels. That leaves the lunar module still attached to this lower part of the slaw. With the top end of the lunar module pointing forward. The command module goes out, turns around, comes back, and docks with the top part of the lunar module. They dock, and then they will hook up some cables and some latches, and they throw a switch in the command module, and that releases the lunar module from the rocket. Now they're going on their way to the moon.

Now, the moon's up here. They're down here three days away almost. They, the spacecraft moon's moving like. So they will follow a trajectory and go around the leading edge of the moon. Fire that service module engine. Slow them down. Put them in orbit, do their thing, and then they use the service module to get away.

When we shut down the stage, we're going 24,500 miles an hour. We're only a few hundred miles above the earth, so Earth's gravity is slowing them down very quick. By the time the crew separates, this thing is probably, everything is probably slowed down to maybe twelve, 14,000 miles an hour because you're still very close to the earth. Earth's gravity is saying, come on back home, guys. So this thing, now, when they separate, they would slow, this would slow this stage down maybe 7 miles an hour, 8 miles an hour.

They would speed up the spacecraft a few miles an hour. And the reason is so much momentum with this. If we did not slow this stage down, there was a very high probability that before they could reach the moon, the s ivb stage would run into the spacecraft.

Oh, okay. So this was a safety. So they were, they may be flying in formation anyway. Well, you're going, I mean, you know, you're going in this, going to the same place if you don't do something. So we would make a, that was a safety measure. How would you fire? Where would the rockets at? That's that auxiliary propulsion system back there, the little black thing right there.

Okay. Once we had done that maneuver, okay, and everything was okay. Now, depending on the mission, the early missions, what we would do then is we would actually reorient the stage, pump some propellant out the back of it. That's left, a little bit of propellant left. Fire the engine, just pump it out of it, fire some thrusters. And the moon's up here, so we'll slow it. We're going, let's say, we're going 12,000 miles an hour. We slow this thing 85 miles an hour out of 12,000, it will go around the trailing edge of the moon.

Really, we get within 2000 miles of the moon, the moon's gravity. Now throw this in orbit around the sun. So we got five of these orbiting the sun right now. Right now. Now, beginning with Apollo twelve, the astronauts would leave instrument packages on the moon called Apollo lunar surface experiment package. One of the science objectives of Apollo was to determine what the interior of the moon, what's the consistency? Does it have a molten core like the Earth? Is it sort of like a consistent density? Or does it have mass concentrations, which it turns out it does.

So beginning with Apollo 13 after twelve, and every time they land, they leave an LSet package. So at Apollo 13, instead of slowing at 85 miles an hour, we slow at 45 and slam it into the moon. This thing hitting the moon is about somewhere around ten to eleven tons of TNT. What? Create about a two and a half to three-hour moonquake.

It rattled it pretty good. All the green men are running around. Oh, man, the Americans are back. It would be a moonquake, wouldn't it? It's not an earthquake. That's right, a moonquake. And so the computers that you controlled to fire that package, the AP's right there. So this computer would control that AP's.

And instead of 85 miles an hour deceleration, you'd give it. What'd you say, 45? Yeah. Just how many seconds do I burn? And so there was a conversation. Hey, computer team, we need you to fire this much so we can slam this into the moon. These were all pre-programmed and pre-planned.

So this is a little loud because the air conditioning unit back there. But this is what you worked on? Yes. The instrument unit sits on top of the third stage. Basically, the thing is set up like this so that you can distribute your weight around the outside of the thing. And control your center of gravity and so forth. You know, the hope was that we would go on with an Apollo application program.

And with this layout like this, with the different thermal conducting panels, we could move equipment around and, you know, do different experiments. So this thing sat on top of the third stage. And controlled the whole rocket? That's right. Those lines up at the top up there, you see going down, those were the lines that went down, connected the other stages to allow us to communicate with them.

That's awesome. And there were methods in the system for separation to disconnect the cables. And we made another video about the computer over there. That's a whole different thing, isn't it? Yeah. So I guess if you want to learn more about the computer for Saturn five, you should just go watch that video. I guess so. When you look at this thing right here. So this is the computer, the instrumentation ring, right?

Yeah. What do you feel when you see this? What do I feel? Yeah. Nothing. Yeah, I've been there before. Well, it's. You know, it brings back a lot of good memories. I know that because this was. So many of us that came in to work on this program were right out of college. So this is something that nobody had ever done before.

And it was a great learning experience because there's so many different aspects to it. Technology goes from the RF technology to transmit the data to the ground. The telemetry systems and so forth. The environmental control system. So did you feel like a pioneer? I just felt like somebody who didn't know what the heck was going on. I got out. I finished college in 1965. Okay.

I had had zero computer courses of any kind. No digital anything. It was all analog. In fact, all my stuff was high. Was like, TVA power, you know, high. Biggest power stuff. So I came here and had to learn a whole nother world. But this is a point that, in my mind, it's kind of sad that it hasn't been promoted more.

When this program was at its peak, there were 300,000 contractors and 47,000 nasa employees working on this thing. Well, a lot of us contractors had come from college and we had come into this, a lot of young folks working on these programs. The things that we learned in this. Then we moved, you know, after these programs phased down, most of us went off to other. Other fields. So I started with this and doing flight evaluation and so forth and, you know, systems and component issues, trying to work through what happened.

Then this all ended. We did the computer and the control system for Skylab worked on that. We had a 24 hours, seven-day a week mission support tied in with Houston from our facility here in Huntsville. And then this all really phased down. NASA was getting budget cuts and not really sure where to go with shuttle. So a lot of us went to other things.

I worked on a Patriot missile program for several years and then IBM closed here. And we went to North Carolina in the commercial side of IBM, applying what I learned, a lot of what I learned here. Then they decided, well, we need some engineers that can know some computer science. So they sent us back to get a computer science degree. So my last job at IBM was I writing software to read handwritten amounts off personal checks.

Really, that was the first, probably one of the first widespread commercial applications of machine learning that was ever done. That was terrific. Fun job. So you went from. You went from some of the first transistors ever, right, to machine learning in your career. Yep. What's that like? It's pretty neat.

And then I retired from IBM after 31 years, moved back to Hunts Hill, spent another 19 years working on Patriot again. Wow. I had 51 year career. That's amazing. Yeah. Let's talk about one more thing here where we talked about when the crew separated, went on their way, then we targeted. We slowed this stage down and targeted the moon and tried to throw it in orbit. Let's go to Apollo twelve.

Apollo twelve was absolutely one of the. An engineer's dream. There were more crazy things happening on that one than you can imagine we're trying to send this thing 2000 miles past the trailing edge to get thrown into solar orbit. On Apollo twelve, the tracking system was such that they thought they were going faster than they actually were, so they slowed it down another 25 miles an hour beyond what was already programmed.

Well, turns out we missed the moon several thousand miles. It goes into very, very high orbit about the Earth, something like a 70,000 miles by maybe 500,000 miles something. It really is very high orbit. Well, over the next several years, this thing, apparently, as it's going in this orbit, is getting affected by the Earth's gravity and the moon's gravity. So the orbit slowly gets stretched.

Well, there's a point called Lagrange L, one point where the gravity of the moon, I mean, the gravity of the sun and the gravity of the earth equal earth's pulling this way, the same amount as the sun's pulling that way. Well, the people that I believe is JPL, they believe that this thing's orbit stretched out to the point that it went beyond the L one point and was ultimately pulled into orbit around the sun after all. So this thing goes out there and he orbits the sun.

Of course, everybody said, oh, well, we knew that would happen. Anybody believe that? So about 30 years later, 2002, amateur astronomer sees this white dot, goes on the Internet, reports that he thinks this is an asteroid. Whatever, JPL and I think MIT people start looking at it and scratching their heads, no, the trajectory can't be an asteroid.

And I believe it's this doctor Paul Chotis at JPL. Their group started looking at it, and they are the people who track space junk. And he said that he had done some back figuring and thought this was actually the third stage from Apollo twelve, and it was coming back into orbit around it, Earth, in 2002, 2002, wow.

So this Lagrange point follows the Earth around the sun. Okay, this thing had gotten into some orbit or about the sun, and it's just, you know, it's going to stay in that same pretty well orbit. It may precess a little bit for the most part. So this Lagrange point now is following the Earth.

Well, at this point in time, S IVB, the earth, and the Lagrange point just happen to be at the right point. And this thing gets S IVB, an instrument unit, gets pulled back into orbit around the Earth. So it orbits the earth for about a year, gets near the moon on one of these orbits, and gets thrown back into solar orbit again.

Now, the people at JPL said they think this is going to happen again will re-happen about every 40 years for the next thousand or 2000. Ultimately it'll run into the earth or the moon. And that's all because this little module right here, the AP's on the back of the third stage, fired just a little bit. 25 mph too much. Yeah. And that put this thing in, started all this foolishness.

Right, so it started all this foolishness. Yeah. Right. So this guy is still floating around. If you want to know about it, you can go out on the Internet and do an Internet search on J zero zero two E three. That's the space junk number for this thing.

And there is a. There are a couple of people have put plots of what the JPL simulation is that shows this thing coming around L one, orbiting the earth. And you can see every time it gets close to Earth, you can see how shape of the orbit changes. And then on this last one, it comes around and the moon just grabs it and throws it out into orbit.

But my grandkids will see it again. I could. That's amazing. That's awesome. Some poor slob, 2000 years now, gonna be walking down the street, see this shadow getting big, real big, real quick. Smashing. I wonder what that was. That's amazing.

All right, Luke, you've talked a lot about the rocket, all three stages, the instrumentation ring here, and then we get up to this business up here. I noticed you don't talk a lot about this side over here.

Well, yeah, well, we were the rocket guys. That was our part. You were like a tractor. Yeah, that's right. You hauled them up there. That's right. And then. So Johnson would handle most of this? Yeah. Well, the Johnson space from the instrument unit forward is all Johnson space station.

Those are responsible for all of that. So your job was done and how much time once you know, from T zero to how well the instrument unit would last about eleven to 12 hours, the batteries would run down. So after that, we couldn't do anything else. That was our part. We got them on their way and we got this thing heading either in solar orbit or we're going to crash it into the moon, one of the two. And then that was, you know, the launch vehicle.

Pretty well done, all it can do.

So what did it feel like when you saw Neil Armstrong step out of the. Out of the spacecraft? Pretty cool. I think the biggest problem was my daughter was sitting in front of the TV and I couldn't see, really, Carmen, move over a little bit. And that was, I think I. We all kind of just, wow. Can't believe this.

And you were part of it? Oh, yeah. Yeah. Had a little bit. A little piece of it.

Technology, Inspiration, Science, Apollo Program, Space Exploration, Rocket Engineering, Smartereveryday