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Space Science

First Public Shuttle Engine Test 14

Guppy06 writes: "NASA's John C. Stennis Space Center (Mississippi, near the gulf coast) will be opening its doors to the public for the first time this Saturday. As part of its celebrations of the 20th anniversary of the first space shuttle launch (as well as flight-certifying a Pratt & Whitney fuel turbo pump), there'll be a 520-second static test of an SSME around 2000 CDT. Translating that into English for the non space geeks, that means they'll be lighting up a space shuttle main engine (attatched to a large steel frame, grounded in a big chunk of concrete so it doesn't go anywhere) for about 9 minutes around 8:00. The press release is available here. Now if only they did stuff like this more often, there might be more interest in NASA ..."
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First Public Shuttle Engine Test

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  • by Anonymous Coward
    Who cares about the position of the Earth right after the push? The main thing happening is a change of velocity of v=a*520. The difference in position is then a function of time, roughly x(t) = v*t. (think t = days or weeks)

    ...That's assuming we forgot about the engine exhaust going the other way that will hit air molecules which in turn will hit other air molecules, etc, until the exhaust momentum is ultimately transfered to the Earth.

    I didn't want to write anything long because your posts will get archived while mine will disappear (unless you quote what I say). But given the effort that you put, I think that you deserve something in return.

    You're not hopeless. You're quite knowledgeble, and you can undoubtedly solve many physics problems involving mass, momentum, and the like. But that's not enough. To be a Jedi, you need the feel conservation of energy and conservation of momentum as second nature. These are the two most important concepts in mechanics, and will save your butt countless times.

    You mentioned 5 other things to take into account, and accurately said that it wasn't an exhaustive list, but sometimes there's a trick. If I ask you what is (exp(sin(Pi/9))+sqrt(17+log(23))) - (exp(sin(Pi/9))+sqrt(17+log(23))), you're still busy parsing the first few calculations while anyone with a global view will immediately say this is equal to zero, without even worrying whether I meant log base-10 or base-e.

    Same here. In the rocket engine problem, you put a big box around the Earth such that the boundary of the box will be space. That's a closed system. The total momentum inside of that box doesn't change, as long as nothing gets out of the box (which is the case since I chose a large box, going halfway to the moon, say). Conservation of linear momentum says that the integral of density(x,y,z)*velocity(x,y,z) over that box remains a constant, unchanged by rocket engines, volcanos, or people jumping up and down.

    Now you can say "ah ha but I don't count people or the air to be part of Earth". Fine, but you still have: integral of density(x,y,z)*velocity(x,y,z) over the Earth + integral of density(x,y,z)*velocity(x,y,z) over not-Earth = constant. In other words, the average velocity of the Earth times Earth's mass + the average velocity of the non-Earth times non-Earth is a constant. But these two average velocities are equals, else the Earth and people would be spreading apart and be completely separated given enough time. It really makes no difference if you don't count people and air, as long as people and air don't fly off the Earth.

    The upshot: Earth's orbit won't change at all, and you don't need to worry about the deformation of the steel frame and concrete block or anything else to get that answer. That is why you should worship conservation of momentum as your new God.

  • ...and since I have no mod points today, I'll do my bit by quoting the entire post. It's not my post, I'm quoting an AC.

    This is it:

    Who cares about the position of the Earth right after the push? The main thing happening is a change of velocity of v=a*520. The difference in position is then a function of time, roughly x(t) = v*t. (think t = days or weeks)

    ...That's assuming we forgot about the engine exhaust going the other way that will hit air molecules which in turn will hit other air molecules, etc, until the exhaust momentum is ultimately transfered to the Earth.

    I didn't want to write anything long because your posts will get archived while mine will disappear (unless you quote what I say). But given the effort that you put, I think that you deserve something in return.

    You're not hopeless. You're quite knowledgeble, and you can undoubtedly solve many physics problems involving mass, momentum, and the like. But that's not enough. To be a Jedi, you need the feel conservation of energy and conservation of momentum as second nature. These are the two most important concepts in mechanics, and will save your butt countless times.

    You mentioned 5 other things to take into account, and accurately said that it wasn't an exhaustive list, but sometimes there's a trick. If I ask you what is (exp(sin(Pi/9))+sqrt(17+log(23))) - (exp(sin(Pi/9))+sqrt(17+log(23))), you're still busy parsing the first few calculations while anyone with a global view will immediately say this is equal to zero, without even worrying whether I meant log base-10 or base-e.

    Same here. In the rocket engine problem, you put a big box around the Earth such that the boundary of the box will be space. That's a closed system. The total momentum inside of that box doesn't change, as long as nothing gets out of the box (which is the case since I chose a large box, going halfway to the moon, say). Conservation of linear momentum says that the integral of density(x,y,z)*velocity(x,y,z) over that box remains a constant, unchanged by rocket engines, volcanos, or people jumping up and down.

    Now you can say "ah ha but I don't count people or the air to be part of Earth". Fine, but you still have: integral of density(x,y,z)*velocity(x,y,z) over the Earth + integral of density(x,y,z)*velocity(x,y,z) over not-Earth = constant. In other words, the average velocity of the Earth times Earth's mass + the average velocity of the non-Earth times non-Earth is a constant. But these two average velocities are equals, else the Earth and people would be spreading apart and be completely separated given enough time. It really makes no difference if you don't count people and air, as long as people and air don't fly off the Earth.

    The upshot: Earth's orbit won't change at all, and you don't need to worry about the deformation of the steel frame and concrete block or anything else to get that answer.

    That is why you should worship conservation of momentum as your new God.

  • This kind of even is good for future generations of engineers and scientists. Even if they don't decide they would like to work for NASA, this is the type of event that will ignite a desire to learn about science in children, and hopefully it will encourage parents to help their children learn.
  • by grammar nazi ( 197303 ) on Thursday April 19, 2001 @06:18PM (#277952) Journal
    Can we bring marshmallows and skewers?

    Guppy06 - please spell check.

  • by Vuarnet ( 207505 ) <luis_milan@@@hotmail...com> on Thursday April 19, 2001 @10:22PM (#277953) Homepage
    Tour guide: On your left, we have the Research Building, the restrooms and the caffeteria. On your right...

    FWOOSH!

    Tour guide: Er... we have, or rather had, the souvenir stand. Thanks you all for coming and, uh, here's a free pin for y'all, and please let's keep this a secret betwen ourselves, OK?


    Tongue-tied and twisted, just an earth-bound misfit, I
  • Thanks, everyone. I appreciate the explainations in all their variety. It brings to mind something that my dad told me. He said "If you can't be smart, be funny." I've generally had to live by this advice, now more than ever in the face of such learned dissertations. I thought that I was just asking a humorous question, but apparently it more earth-moving than I realized.
  • How much will this change the orbit of the earth?

    Will having all the people in India stamp their feet for those 9 minutes cancel the effect?

  • "Can we bring marshmallows and skewers?"

    Actually, from what I've heard, there'll be a good deal of water spray. Water makes a good coolant and shock absorber, you know...

    Guppy06 - please spell check.

    Where's the fun in that? And what's the point in spell-checking when /. is never going to post it, anyway? Oh, wait a sec...

  • "How much will this change the orbit of the earth?"

    Hrmm... an SSME puts out 1862 kilonewtons of thrust at sea level. The earth is about 5.92E24 kilograms. Newton tells us that the earth will experience an acceleration of 3.15E-19 m/s^2, or 0.000000315 picometers per second per second. Newton also tells us that the 520 second firing time means that the earth will move 0.000425 picometers, or 1.67 trillionths of an inch. Not accounting for the angle the engine will sweep as the earth turns, of course...

    "Will having all the people in India stamp their feet for those 9 minutes cancel the effect?"

    We'll use conservation of momentum. 1862 kilonewtons for 520 s is 9.68E8 kg*m/s.

    Let's say the average person masses in at 75 kilograms and can jump 30 cm up in the air. Newton tells us that they will be leaving the ground at 2.43 m/s. 75 kg moving at 2.43 m/s is 181.9 kg*m/s. We'll assume for simplicity's sake that they can jump once per second. We'll also assume that it's enough time to gently absorb the shock of their landing with their knees, making the momentum change of the landing negligible compared to the jumping.

    At that rate, it will take about 5,322,000 people to counteract the rocket. According to the CIA World Factbook, the nearest match is Denmark's 5,336,394.

    Unfortunately for the Danes, in order to work, they'll have to be jumping on the other side of the world as the engine. Stennis Space Center is located at 30.369 degrees north latitude, 89.613 degrees west longitude. The opposite side of the earth would be 30.369 degrees south latitude, 90.387 degrees east longitude, or about half-way between Bangladesh and Antarctica, in the middle of the Southern Indian Ocean. Only about a 1400 mile swim due east to Perth, Australia, though...

    ---

    Ask a silly question, inspire somebody to give you a serious answer...

  • I should have pointed out that the 5+ million Danes will only have to jump once. If you want a bunch of people jumping for the entire 520 seconds, you'll only need about 10,235 people, roughly the population of Satellite Beach, FL. (Thank you, Google)
  • My calculations considered neither the rocket's exhaust nor the people to be part of the earth, so it's not a closed system. Do you know what a "frame of reference" is?
  • "Since when does picometers/s^2 times s give picometers? Don't try your latest buzzwords with me until you get that straight."

    It's called "normal differential equations."

    Acceleration = a
    Velocity = v
    Displacement = x
    Time = t

    v = dx/dt
    a = dv/dt
    v(0) = 0
    x(0) = 0

    dv = a*dt
    v = integral of a * dt
    v = at + C (something Galileo figured out w/o calculus)
    v(0) = 0
    0 = a*0 + C1
    C1 = 0
    v = at

    dx/dt = at
    dx = at*dt
    x = integral of at*dt
    x = 0.5*at^2 + C2 (something Galileo figured out w/o calculus)
    x(0) = 0
    0 = 0.5*a*0^2 + C2
    C2 = 0
    x = 0.5*at^2

    a(t) = 3.15E-19 m/s
    t = 520 s
    x = 0.5*(3.15E-19 m/s)*(520 s)^2
    x = 4.25E-14 m

    Is that a rigorous enough explaination for you, or do I need to explain what "derivative" and "integral" mean? How about "limit?"

    The only problem I see is that I stated the wrong metric prefix (0.0425 pm), but you failed to mention that. The inch figure still stands (4.25E-14 m = 1.67E-12 in), which suggests that the raw numbers I was using work fine.

    The only real fault you've caught me on so far is momentarily confusing "momentum" with "kinetic energy" during some on-the-fly calculations. If I really wanted to spend time and effort on this problem, I would have taken into account:

    1.) The motion of the earth during the 520 seconds (which is affected by #4, below)

    2.) The deformation of the steel frame and concrete block due to the firing (after finding veritable blueprints of the structure, information on the type of steel and concrete used, as well as the surrounding soil)

    3.) The height of the combustion chamber above sea level (before, during, and after deformation of the frame, producing differential equations for the affects of time on thrust produced)

    4.) The angular momentum imparted on the earth by the deflection of the exhaust gasses by the concrete block (which will require a formula for the curved surface of the block, and a second formula for how the first one changes during firing)

    5.) What kind of gimballing the engine will be going through (if any) during the testing process

    And this is still not an exhaustive list.

    However, if you take such infinite delight in my brainfart of confusing mv with 0.5mv^2, then good for you. I only wish I were so easily amused.

  • by Guppy06 ( 410832 ) on Saturday April 21, 2001 @06:34PM (#277961)
    I don't think the state of Mississippi has seen a larger congegation of people in one place since Vicksburg. They were NOT prepared for the crowd that showed up. Personally, I'd say more people showed up for this than usually show up along NASA Causeway for a shuttle launch.

    The scheduled firing was scheduled for 8:00. I got to the gate around 7:00, and spent the next hour stuck in traffic along the five-mile stretch to the designated parking area. In that traffic jam, most of the lisence plates were from Mississippi and Louisiana. There were plenty from Alabama (70+ miles away), too many for them all to be military. There was even one from Ontario.

    Upon reaching the parking area (where the people trying to organize parking ran out of designated space), I joined the crowd of 400-500 people waiting on about 4-5 busses (and I only saw one bus owned and operated by NASA). 8:00 came and went with no firing, and around 8:45 (still in line for a bus) somebody started moving through the crowd with a bullhorn saying something about "indefinately postponed" because of technical difficulties.

    I can't really blame them for not expecting the turnout they got. I don't know how well the press release was covered in the Biloxi area, but I know that the bit barely got three paragraphs in some sidebar in New Orlean's Times-Picayune. I guess everybody wanted to get an up-close view of part of that thing that sets off everybody's car alarm whenever it comes in for a landing.

    There's been no official word that I can see yet when they'll try again, and whether it will be public again or not.

    All in all, anybody who think Americans don't care about their space program deserves to get smacked hard.

  • Hey, who needs a souvenir stand? I'll take the engine, thank you very much.

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