Author Topic: SpaceX Falcon 9 : CRS-16 (Dragon SpX-16) : December 5, 2018 - DISCUSSION  (Read 255667 times)

Offline jpo234

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https://twitter.com/cygnusx112/status/1072541873724710913

Quote
The CBI truck backed up to the #Falcon9 and connected into the rear. They must be draining something before moving to the transporter. #SpaceX

For those wondering: CBI is Cliff Berry, Inc.
One of the services they provide is Marine & Onshore Tank Cleaning. This makes me think that they are draining RP1 contaminated sea water.
« Last Edit: 12/11/2018 06:45 pm by jpo234 »
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Offline llanitedave

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He's actually right. You could use both the engine bell and the exhaust volume inside it as an impromptu "reaction wheel" by constantly actuating in a circular matter. And since the gas volume is being continuously expelled it even acts a bit like a yoyo despin-weight in fluid form, so it would be able to give a continuous rotational force without saturating. You rotate a gas volume relative to the core, then get rid of it. (The resulting gas jet would have spiral shape and expand away from the core)

The effect is going to be miniscule and orders of magnitude below the aerodynamic effect of the grid fins or the effects achievable if the rotation axis goes NOT through the gimbal bearing. But if you were in vacuum and this is the only effect you can use, it might actually work.

It has no practical application to this particular core landing, but I don't think you can completely neglect it in vacuum. ;)


The gas generator also contributes a small amount of thrust, and it is off center.  So the combined thrust vector can actually have a slight effect on cancelling roll.
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Offline ellindsey

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He's actually right. You could use both the engine bell and the exhaust volume inside it as an impromptu "reaction wheel" by constantly actuating in a circular matter. And since the gas volume is being continuously expelled it even acts a bit like a yoyo despin-weight in fluid form, so it would be able to give a continuous rotational force without saturating. You rotate a gas volume relative to the core, then get rid of it. (The resulting gas jet would have spiral shape and expand away from the core)

The effect is going to be miniscule and orders of magnitude below the aerodynamic effect of the grid fins or the effects achievable if the rotation axis goes NOT through the gimbal bearing. But if you were in vacuum and this is the only effect you can use, it might actually work.

It has no practical application to this particular core landing, but I don't think you can completely neglect it in vacuum. ;)


The gas generator also contributes a small amount of thrust, and it is off center.  So the combined thrust vector can actually have a slight effect on cancelling roll.

Unless I'm mistaken, the gas generator and its exhaust are stationary on the Merlin 1D.  Only the combustion chamber and nozzle move.  That's certainly the way it appears from looking at the engine, and the hole in the insulation plate around the engine doesn't seem to allow the turbopump exhaust to move.

Offline Zpoxy

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If we're heading down the road of thruster thrust be mindful that its proportional (or at least related) to tank pressure and whatever pressure was available during the flip maneuver is likely to be significantly reduced by the time it gets close to landing in a normal landing and in this case where there was an ongoing battle between grid fins and thrusters I'd expect the pressure to be lower than what the designers had hoped for in their lowest pressure scenario.  Or not, maybe the tanks are vastly larger than necessary.

Are you assuming the cold gas thrusters are connected directly to the supply tank? I'm sure there is a pressure regulator between the supply tank and the thrusters. Providing a relatively constant pressure and thrust until the tank goes flat.

Offline Scylla

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Doing The Math On The Spinning Falcon 9 Booster
Scott Manley

Published on Dec 11, 2018
How much does deploying the landing legs change the rotation?
Let's run the numbers.
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Offline Rocket Science

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The stage landed at an angle so the final "coup de gras" arresting rotation was from one possibly two legs striking the water...
"The laws of physics are unforgiving"
~Rob: Physics instructor, Aviator

Offline Kabloona

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Doing The Math On The Spinning Falcon 9 Booster
Scott Manley

Published on Dec 11, 2018
How much does deploying the landing legs change the rotation?
Let's run the numbers.


Shorter Scott Manley for those who don't watch the video:

Leg deployment roughly doubles the roll moment of inertia.
So leg deployment by itself will reduce roll rate by about half.
(But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters)

Graphical analysis of video shows RCS thrusters are in fact reducing roll rate *before* leg deployment.
Then leg deployment further reduces roll rate by increasing MOI.
But roll rate is not fully nulled before legs hit water.
Legs hitting water may have been the final factor in nulling the roll rate.

Hope I got that more or less correct. Thanks, Scott.
« Last Edit: 12/12/2018 01:45 am by Kabloona »

Offline Jdeshetler

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I didn't expected that my twitter from Dec 6th to Scott would started this debate but that was cool!

https://twitter.com/jdeshetler/status/1070773216413605889

Offline Rocket Science

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Doing The Math On The Spinning Falcon 9 Booster
Scott Manley

Published on Dec 11, 2018
How much does deploying the landing legs change the rotation?
Let's run the numbers.


Shorter Scott Manley for those who don't watch the video:

Leg deployment roughly doubles the roll moment of inertia.
So leg deployment by itself will reduce roll rate by about half.
(But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters)

Graphical analysis of video shows RCS thrusters are in fact reducing roll rate *before* leg deployment.
Then leg deployment further reduces roll rate by increasing MOI.
But roll rate is not fully nulled before legs hit water.
Legs hitting water may have been the final factor in nulling the roll rate.

Hope I got that more or less correct. Thanks, Scott.
Scott's a good guy.
"The laws of physics are unforgiving"
~Rob: Physics instructor, Aviator

Offline graywolf

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>>> But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters

This scratched my ears first time when I watched Scott's video and now it is on NASA forum.
IMO, this is not correct.

Remember momentum conservation law.

The speed of rotation has slowed down 1/2x, because MOI doubled after legs were deployed, so for the body to keep the same momentum, the speed of rotation should be halved.

RCS should fight against F9's momentum. It does not matter if legs are deployed or not. The momentum is the same (well provided we do not have any more forces adding to rotation, which in case of deployed legs is probabaly negative, that is the legs are slowing rotation down due to air resistance, and then due to water resistance).

My point is: RCS effectiveness in roll elimination have not changed with legs deployment.

Online meekGee

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>>> But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters

This scratched my ears first time when I watched Scott's video and now it is on NASA forum.
IMO, this is not correct.

Remember momentum conservation law.

The speed of rotation has slowed down 1/2x, because MOI doubled after legs were deployed, so for the body to keep the same momentum, the speed of rotation should be halved.

RCS should fight against F9's momentum. It does not matter if legs are deployed or not. The momentum is the same (well provided we do not have any more forces adding to rotation, which in case of deployed legs is probabaly negative, that is the legs are slowing rotation down due to air resistance, and then due to water resistance).

My point is: RCS effectiveness in roll elimination have not changed with legs deployment.
Leg touching water, that I obviously buy.

Maybe that's why one leg was lost, too.

Did they ever fish it out?  I mean they have the exact surface coordinate, and a good estimate of surface currents...



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Offline Kabloona

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>>> But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters

This scratched my ears first time when I watched Scott's video and now it is on NASA forum.
IMO, this is not correct.

Remember momentum conservation law.

The speed of rotation has slowed down 1/2x, because MOI doubled after legs were deployed, so for the body to keep the same momentum, the speed of rotation should be halved.

RCS should fight against F9's momentum. It does not matter if legs are deployed or not. The momentum is the same (well provided we do not have any more forces adding to rotation, which in case of deployed legs is probabaly negative, that is the legs are slowing rotation down due to air resistance, and then due to water resistance).

My point is: RCS effectiveness in roll elimination have not changed with legs deployment.

You are correct insofar as conservation of momentum is concerned, ie for a given quantity of stored angular momentum, the RCS thrusters will have to impart a constant amount of angular impulse (torque x time) to null it out, regardless of leg position.

But Scott's point was that  a fixed RCS thrust will impart less angular acceleration to the rocket with the legs extended. That is what he meant by "reduced effectiveness."

And he may have been of the mind that some aerodynamic force, although reduced, may still have been inducing roll torque through the grid fins, so the RCS thrusters may still have been fighting the grid fins, not just stored angular momentum. In which case, their "effectiveness", ie induced angular acceleration for an RCS pulse of given duration, would indeed be reduced.

You are both correct, but emphasizing different points.
« Last Edit: 12/12/2018 03:04 pm by Kabloona »

Online meekGee

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>>> But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters

This scratched my ears first time when I watched Scott's video and now it is on NASA forum.
IMO, this is not correct.

Remember momentum conservation law.

The speed of rotation has slowed down 1/2x, because MOI doubled after legs were deployed, so for the body to keep the same momentum, the speed of rotation should be halved.

RCS should fight against F9's momentum. It does not matter if legs are deployed or not. The momentum is the same (well provided we do not have any more forces adding to rotation, which in case of deployed legs is probabaly negative, that is the legs are slowing rotation down due to air resistance, and then due to water resistance).

My point is: RCS effectiveness in roll elimination have not changed with legs deployment.
The rate of decrease of angular momentum will remain the same after legs are deployed. if

The rate of decrease of rotation rate (which is prolly what we mean by "effectiveness") will be lower once the legs are out.

So here's a riddle:  if you had X amount of stored gas, and ignoring the grid fins for a second - would you want to expend it before or after leg deployment?

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Offline Jim

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If the control system didn't take that into account, they'd get unexpected spin during engine operation.


That is what RCS is for.

Offline Rocket Science

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>>> But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters

This scratched my ears first time when I watched Scott's video and now it is on NASA forum.
IMO, this is not correct.

Remember momentum conservation law.

The speed of rotation has slowed down 1/2x, because MOI doubled after legs were deployed, so for the body to keep the same momentum, the speed of rotation should be halved.

RCS should fight against F9's momentum. It does not matter if legs are deployed or not. The momentum is the same (well provided we do not have any more forces adding to rotation, which in case of deployed legs is probabaly negative, that is the legs are slowing rotation down due to air resistance, and then due to water resistance).

My point is: RCS effectiveness in roll elimination have not changed with legs deployment.
Welcome to the forum! :) The mass is conserved but the distribution has changed and so has the angular velocity. The RCS will lose some effectiveness do to having to act from a shorter lever arm relative to the tip of the extended legs...
https://www.grc.nasa.gov/www/k-12/airplane/angdva.html
"The laws of physics are unforgiving"
~Rob: Physics instructor, Aviator

Offline Kabloona

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>>> But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters

This scratched my ears first time when I watched Scott's video and now it is on NASA forum.
IMO, this is not correct.

Remember momentum conservation law.

The speed of rotation has slowed down 1/2x, because MOI doubled after legs were deployed, so for the body to keep the same momentum, the speed of rotation should be halved.

RCS should fight against F9's momentum. It does not matter if legs are deployed or not. The momentum is the same (well provided we do not have any more forces adding to rotation, which in case of deployed legs is probabaly negative, that is the legs are slowing rotation down due to air resistance, and then due to water resistance).

My point is: RCS effectiveness in roll elimination have not changed with legs deployment.
Welcome to the forum! :) The mass is conserved but the distribution has changed and so has the angular velocity. The RCS will lose some effectiveness do to having to act from a shorter lever arm relative to the tip of the extended legs...
https://www.grc.nasa.gov/www/k-12/airplane/angdva.html

Graywolf is correct as far as he goes. Assuming a fixed quantity of stored momentum, it will take the same amount of RCS total angular impulse (torque x time) to zero out that angular momentum.

The only difference between legs closed or legs extended, in the ideal case, is that with legs closed the stage is rolling faster with lower MOI, and with legs extended the stage rolls slower with higher MOI. But since total angular momentum remains the same (MOI x roll rate), in each case the RCS thruster will need a burn of the same duration to cancel out the spin.

The RCS thrusters don't know nor care where the angular momentum is "stored" on the stage. But as long as that quantity remains fixed, a fixed torque applied for a fixed duration will null it out.

But, yes, the RCS thruster torque will induce less angular acceleration with legs extended, due to increased MOI.
« Last Edit: 12/12/2018 03:06 pm by Kabloona »

Offline Rocket Science

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>>> But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters

This scratched my ears first time when I watched Scott's video and now it is on NASA forum.
IMO, this is not correct.

Remember momentum conservation law.

The speed of rotation has slowed down 1/2x, because MOI doubled after legs were deployed, so for the body to keep the same momentum, the speed of rotation should be halved.

RCS should fight against F9's momentum. It does not matter if legs are deployed or not. The momentum is the same (well provided we do not have any more forces adding to rotation, which in case of deployed legs is probabaly negative, that is the legs are slowing rotation down due to air resistance, and then due to water resistance).

My point is: RCS effectiveness in roll elimination have not changed with legs deployment.
Welcome to the forum! :) The mass is conserved but the distribution has changed and so has the angular velocity. The RCS will lose some effectiveness do to having to act from a shorter lever arm relative to the tip of the extended legs...
https://www.grc.nasa.gov/www/k-12/airplane/angdva.html

No, graywolf is correct as far as he goes. Assuming a fixed quantity of stored momentum, it will take the same amount of RCS total angular impulse (torque x time) to zero out that angular momentum.

The only difference between legs closed or legs extended, in the ideal case, is that with legs closed the stage is rolling faster with lower MOI, and with legs extended the stage rolls slower with higher MOI. But since total angular impulse remains the same (MOI x roll rate), in each case the RCS thruster will need a burn of the same duration to cancel out the spin.

The RCS thrusters don't know nor care "where" the angular momentum is stored on the stage. But as long as that quantity remains fixed, a fixed torque applied for a fixed duration will null it out.
Here is a good explanation of "my madness"... ;D
https://www.quora.com/What-is-the-difference-between-angular-momentum-and-angular-velocity
"The laws of physics are unforgiving"
~Rob: Physics instructor, Aviator

Offline Kabloona

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Yes, I think we all understand high school physics. can we move on now?  :)

Offline whitelancer64

>>> But increased MOI from leg deployment reduces effectiveness of RCS roll thrusters

This scratched my ears first time when I watched Scott's video and now it is on NASA forum.
IMO, this is not correct.

Remember momentum conservation law.

The speed of rotation has slowed down 1/2x, because MOI doubled after legs were deployed, so for the body to keep the same momentum, the speed of rotation should be halved.

RCS should fight against F9's momentum. It does not matter if legs are deployed or not. The momentum is the same (well provided we do not have any more forces adding to rotation, which in case of deployed legs is probabaly negative, that is the legs are slowing rotation down due to air resistance, and then due to water resistance).

My point is: RCS effectiveness in roll elimination have not changed with legs deployment.
Leg touching water, that I obviously buy.

Maybe that's why one leg was lost, too.

Did they ever fish it out?  I mean they have the exact surface coordinate, and a good estimate of surface currents...



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ABCD: Always Be Counting Down

Yes, the leg was removed by divers the first day that the booster was floating outside Port Canavera.
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Offline Rocket Science

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Yes, I think we all understand high school physics. can we move on now?  :)
College level... ;) How about: Saltwater intrusion and re-use? ??? ;D
« Last Edit: 12/13/2018 02:29 pm by Rocket Science »
"The laws of physics are unforgiving"
~Rob: Physics instructor, Aviator

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