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Old 24-March-2008, 02:41 PM
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Default Restarting of Liquid Fueled Rocket Engines

A friend recently leant me a copy of the Spacecraft Films production of "The Mighty Saturns." It contains lots of footage of Saturn rocket launchs from many angles, including inside the fuel tanks. With a camera mounted at the top of the tank, you can see the fuel drop very quickly as it is consumed by the engine(s). Once the engine shuts off, there is a sudden "whiplash effect" as the fuel is exposed to no acceleration forces. Blobs of fuel begin to float all around the inside the tank.

I know that the lower stages of the Saturn were one-time fire stages, but the third stage of the Saturn 5 had to be restarted. How was the engine restarted with the fuel flopping around inside the tank as blobs? I would imagine that unless the unused fuel was forced to the drain opening of the tank, the engine would get a mixture of liquid and gaseous fuel, which would probably be a bad thing.

I guess this question applies to any liquid-fueled engine that has to be started in "weightlessness." How do rocket engineers keep the fuel near the drain of the tank?
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Old 24-March-2008, 04:16 PM
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One solution is ullage motors (Wikipedia) to provide artificial gravity.

Quote:
The four ullage motors of the Saturn V rocket used in the American Apollo program were located on the second stage. In the third stage (known as S-IVB), there was a more general Auxiliary Propulsion System that also had ullage functions.
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Old 25-March-2008, 05:52 PM
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Don't know about Saturn rockets, but hydrazine and nitrogen tetroxide tanks on Russian spacecraft usually contain what amounts to a nitrogen-filled balloon under pressure. As fuel gets used up, the balloon expands and keeps forcing the fuel against the intake valve; there is no free gas in the tank. I don't think this works with cryogenic fuels though -- no elastic substance retains its elasticity in contact with liquid hydrogen.
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Old 25-March-2008, 06:30 PM
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Don't know about Saturn rockets, but hydrazine and nitrogen tetroxide tanks on Russian spacecraft usually contain what amounts to a nitrogen-filled balloon under pressure. As fuel gets used up, the balloon expands and keeps forcing the fuel against the intake valve; there is no free gas in the tank.

That technique is very common for satellites that use hypergolic propellants (that's almost all of them).

One solution is ullage motors (Wikipedia) to provide artificial gravity.

A more accurate way to say that is that the ullage motors cause a small acceleration that causes the propellants to shift towards the rear of the tanks. The acceleration mimics the effects of gravity but isn't really artifical gravity.

I know that the lower stages of the Saturn were one-time fire stages, but the third stage of the Saturn 5 had to be restarted. How was the engine restarted with the fuel flopping around inside the tank as blobs? I would imagine that unless the unused fuel was forced to the drain opening of the tank, the engine would get a mixture of liquid and gaseous fuel, which would probably be a bad thing.

From this source:

One second after first stage separation, eight solid-fueled motors mounted on the first/second stage adapter ring were fired for four seconds. These provided a combined thrust of 181,000 pounds.

In addition to maintaining the positive motion of the rocket, these motors performed an ullage maneuver, forcing the second stage fuel to the bottom of its tanks in order to feed the engines. The five J-2 second stage engines were fired during this ullage burn.

...

At this point, the Saturn V had achieved a speed of 15,700 m.p.h. and an altitude of 115 miles.

Two solid-fueled ullage motors located 180 degrees apart on the third stage aft skirt were fired for four seconds to settle the liquid fuel. These motors produced 6,800 pounds of thrust.

Three seconds after second stage separation, the S-IVB third stage J-2 engine was ignited. Nine seconds later, the third stage ullage motors which fired at separation and their cases were jettisoned.

The third stage J-2 engine was fired for 142 seconds before being shut down. This initial S-IVB burn was sufficient to carry the Apollo spacecraft into a 118-mile orbit at a speed of 17,500 m.p.h.

At the end of this first S-IVB burn, two ullage motors were fired to settle the remaining fuel and provide spacecraft stabilization. These ullage motors were housed in two Auxiliary Propulsion System (APS) modules located 80 degrees apart on the third stage aft skirt.

Each APS module housed three attitude control motors and one ullage motor. The attitude control motors could each produce 150 pounds of thrust, while the ullage motors could each produce 70 pounds of thrust. All burned nitrogen tetroxide/hydrazine liquid fuel.

During two or three checkout orbits, the S-IVB attitude control motors could be fired in sequence to make any necessary on-orbit corrections. Following these checkout orbits, the ullage motors were fired for 77 seconds to settle the fuel and provide forward spacecraft momentum.
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Old 25-March-2008, 06:48 PM
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Quote:
Originally Posted by Larry Jacks View Post
The acceleration mimics the effects of gravity but isn't really artifical gravity.
Like, what do you consider real artificial gravity?

Wikipedia: Artificial gravity:

Quote:
Artificial gravity could be created in several ways:
[...]
Acceleration
The spacecraft could, in theory, continuously accelerate in a straight line, forcing objects inside the spacecraft in the opposite direction of the direction of acceleration.
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Old 25-March-2008, 06:54 PM
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The effect is caused by acceleration, not gravity (artificial or otherwise).
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Old 25-March-2008, 07:03 PM
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Quote:
Originally Posted by Larry Jacks View Post
The effect is caused by acceleration, not gravity (artificial or otherwise).
Of course the effect is not real gravity. It's artificial, right?

If acceleration cannot produce artificial gravity, what is something that you do consider to do so. What makes the one real artificial gravity and the other -- what? -- ersatz artificial gravity?

What's wrong with the Wikipedia usage? How would you fix it?

(Next up: margarine -- real artificial butter or... what?)
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Old 25-March-2008, 07:23 PM
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Thanks for the info guys.

BTW: I understood what was meant by "artificial gravity."
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Old 26-March-2008, 12:13 AM
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Fuel-displacing bladders keeps the fuel towards the back. The ullage motors help, but what if there's a misfire due to excessive splashing - now you're out of ullage motors.

I'd opt for both options!

I think I've also seen a design for a bladder which is anchored at both ends and the space between the bladder and the insides of the fuel tank are displaced with nitrogen. Sort of like a toothpast tube, but with less liklihood that the bladder wouldn't be injested into the fuel pump.

That would be bad. Probably fatal, even if it's at the very end of the burn.
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Old 26-March-2008, 12:50 AM
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Quote:
Originally Posted by 01101001 View Post
What's wrong with the Wikipedia usage? How would you fix it?
Change it to "simulated gravity".
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Old 26-March-2008, 01:00 AM
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Quote:
Originally Posted by Noclevername View Post
Change it to "simulated gravity".
I'm guessing that's a joke. From:

http://www.answers.com/topic/artificial

Quote:
SYNONYMS
artificial, synthetic, ersatz, simulated.
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Old 26-March-2008, 01:14 AM
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Quote:
Originally Posted by Van Rijn View Post
I'm guessing that's a joke. From:

http://www.answers.com/topic/artificial
With all due respect to Answers, I think the two words have somewhat different connotations. A thing can be artificial (manmade) and still identical to the "natural" version.

Now if I'd said "Processed Gravity Product", that would be joke. Not much of one, but still...
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Old 26-March-2008, 03:12 AM
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Quote:
Originally Posted by Noclevername View Post
With all due respect to Answers, I think the two words have somewhat different connotations. A thing can be artificial (manmade) and still identical to the "natural" version.
Well, that would be consistent with the equivalence principle. But, anyway, I don't see a useful distinction in this case between "simulated" and "artificial" - which is why I suspected a joke before I googled the synonyms.
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Old 26-March-2008, 10:48 PM
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Quote:
Originally Posted by Van Rijn View Post
Well, that would be consistent with the equivalence principle. But, anyway, I don't see a useful distinction in this case between "simulated" and "artificial" - which is why I suspected a joke before I googled the synonyms.
Simulated means fake-- and that's all it means. Artificial just has to do with whether something's natural, not whether it's real. For example, an "artificial diamond" has the same carbon structure as a natural diamond. It really is a diamond. A "simulated diamond" isn't a diamond at all.
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Old 27-March-2008, 04:49 AM
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Quote:
Originally Posted by Noclevername View Post
Simulated means fake-- and that's all it means. Artificial just has to do with whether something's natural, not whether it's real.
The acceleration due to a rocket isn't real?
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Old 27-March-2008, 01:08 PM
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I don't necessarily want to get into your battle over what qualifies as artificial or simulated, but according to the NOVA website...

Quote:
The key idea of general relativity, called the equivalence principle, is that gravity pulling in one direction is completely equivalent to an acceleration in the opposite direction.
[my emphasis]
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Old 27-March-2008, 03:18 PM
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Quote:
Originally Posted by mugaliens View Post
Fuel-displacing bladders keeps the fuel towards the back. The ullage motors help, but what if there's a misfire due to excessive splashing - now you're out of ullage motors.
Ullage motors are often solid propellant so you don't have this problem.
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Old 27-March-2008, 04:28 PM
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Quote:
Originally Posted by Bob B. View Post
Ullage motors are often solid propellant so you don't have this problem.
Perhaps Mugaliens' point was that the ullage motors are a one-shot deal (because they are solid). If the liquid fuel hasn't settled by the time the ullage motor burns out, you don't get another chance to restart the liquid engine.

Of course, you could always include spare ullage motors, or use a restartable liquid fueled ullage motor that relies on a pressure bladder. (From Larry's link, it appears that the Apollo third stage did that, using hydrazine as the fuel.) With cryogenic fuels used for the main engines, a pressure bladder wouldn't work well because of the cold temperature and tendency for the fuel to boil into a gas.

BTW: To reduce splashing, the Saturn designers added baffles to the fuel tanks. At one point, they tried to reduce fuel sloshing by floating "beer cans" on the surface.
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Old 27-March-2008, 05:49 PM
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Quote:
Originally Posted by Extravoice View Post
Perhaps Mugaliens' point was that the ullage motors are a one-shot deal (because they are solid). If the liquid fuel hasn't settled by the time the ullage motor burns out, you don't get another chance to restart the liquid engine.
Yes, I think I may have misread what he was saying.

Quote:
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Of course, you could always include spare ullage motors, or use a restartable liquid fueled ullage motor that relies on a pressure bladder. (From Larry's link, it appears that the Apollo third stage did that, using hydrazine as the fuel.)
The Saturn third stage used both solid motors and liquid engines for ullage. I believe the solid motors were used prior to the first engine burn only and in combination with the APS (Auxiliary Propulsion System) engines. The APS provided ullage not only at the st