Author Topic: SpaceX Falcon 9 : PAZ & Microsat 2a/2b : SLC-4E : Feb 22, 2018 : DISCUSSION  (Read 207698 times)

Offline wolfpack

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How did the fairing recovery go?

Just sit right back and you'll hear a tale, a tale of a fateful trip....



photoshopped by me

Maybe the “catcher’s mitt” isn’t really needed? Just splash ‘em down softly and fish ‘em out.

Offline 210Tom

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I wonder if I observed one of the satellites from Northern Norway(!).

At 18:10 local time (173 minutes after the launch of the Falcon 9), I observed an object that appeared to be venting propellants or thrusting, moving from southwest to northwest. My brother also observed it from about 70 kilometers away. It was clearly in vacuum or near vacuum due to the pure arcing shape of the plumes. As it moved further north it seemed to change from plumes going straight up and down from the object to one big plume to the right of the object as it moved. So it looked almost like a plane change maneuvre.

Now, the reason why I ask if it might be Paz or one of the other payloads is the math. Wikipedia says 514 km altitude for Pez, which gives an orbital period of almost 95 minutes. So when I observed the object, it would be about 1,8 orbits into the flight.

I live at 69° northern latitude. Vandenberg is at 34°, and the launch headed south (at 97° inclination and not 90°, so forgive my naive calculation). So it headed south 34° to equator, 90° to the south pole, 90° north to equator again and 69° north to where I live. That's (34+90+90+69)=283° to travel around the world from Vandenberg to here. That equals (283/360)=0,79 orbits. So yes, the timing would match about 1,8 orbits into the mission, not accounting for the few minutes it takes for the rocket to reach orbital speed, although my observation at 18:10 was when it appeared south of me, not quite at my latitude yet.

My observation was after sunset with a not-quite dark sky, so the satellite I observed roughly followed the terminator with the sun on its left relative to its direction. Paz launched in the very early morning in California, following roughly the terminator with the Sun to its left.

Does anyone know if any of the satellites did a burn or venting of propellants about 173 minutes after launch time?

Edit: also, Vandenberg is 120° west. That means that in a naive calculation it would go up from antarctica at 60° east. But the Earth rotates, and 173 minutes is about 0,12 days. This means the Earth had time to rotate (360°*0,12)=43°, which means the satellite would be over (60-43)=17 degrees eastern longitude. And hey presto, I live at 18° eastern longitude and observed it fly by from southwest to northwest!

Edit 2: the exact directions were difficult to assess as I stopped my car in the middle of nowhere and so I am not positive that it was west of me. But the calculations are so rough that one should not interpret them as precise in any way, just a back-of-the-napkin ballpark calculation.

Hey All!
Just registered here today to figure out what this was.
I also saw the event last night from flight deck of an airliner. We were over the Baltic sea and saw the object on a roughly northwest path. Very interesting sight indeed as it was quite bright.
Maybe there's a trajectory map over that area anywhere? And the location of where S2 was de orbiting?

Online catdlr

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Quote
Hey All!
Just registered here today to figure out what this was.
I also saw the event last night from flight deck of an airliner. We were over the Baltic sea and saw the object on a roughly northwest path. Very interesting sight indeed as it was quite bright.
Maybe there's a trajectory map over that area anywhere? And the location of where S2 was de orbiting?

the splashdown area for the S2 is located here.  https://forum.nasaspaceflight.com/index.php?topic=44892.msg1788363#msg1788363
It's Tony De La Rosa, ...I don't create this stuff, I just report it.

Offline alexterrell

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https://www.instagram.com/p/BfgRX-lgIt6/

 8)

If it landed so softly, major amounts of sea water shouldn't have touched the inside of the fairing. The outside should be pretty waterproofed, so maybe they can still try to lift it out of the water as an almost-valid recovered fairing?


Otherwise it has the right shape for a fishing boat ;)

Seriously. I wonder what is keeping them from designing it to be seaworthy enough to be towed back to port (or at least float long enough to be winched up onto a barge)?  Seems like an easier engineering problem than a pinpoint parasail landing through random weather into a giant floating net!
That would be my thinking. People say "sea water is bad" but composite structures are pretty good against it. I suspect the micro-thrusters would be more susceptible to damage, but again - alloys are corrosion resistant. And it could be winched up and hosed down within minutes.

I read that this time the fairing missed by several hundred metres. What happens if it misses by 10 metres and hits the cabin?

Offline Mader Levap

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I read that this time the fairing missed by several hundred metres. What happens if it misses by 10 metres and hits the cabin?
My guess: you spend few ten k $ in repairs to boat and write fairing off. Humans inside should be sufficiently protected.
Be successful.  Then tell the haters to (BLEEP) off. - deruch
...and if you have failure, tell it anyway.

Offline kevinof

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It's a carbon composite  fairing (I think) vs a steel hulled boat. I'll go with the boat. Yes it could hit the antenna/radar but if it hits anywhere else the boat is going to win every time.

I read that this time the fairing missed by several hundred metres. What happens if it misses by 10 metres and hits the cabin?
My guess: you spend few ten k $ in repairs to boat and write fairing off. Humans inside should be sufficiently protected.
« Last Edit: 02/23/2018 01:09 pm by kevinof »

Offline garcianc

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Paz launch patch

Translation: "Everything seems impossible until it is accomplished"

Also, I don't remember seeing a SpaceX patch without a clover leaf before, or am I missing it?


edit: better translation
« Last Edit: 02/23/2018 01:02 pm by garcianc »

Offline swervin

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From the article written for this mission, what is the rocket core in the background of the picture mentioning the VAFB landing pad construction?

It appears to have two engines? Maybe something previously discussed?

-Splinter

Offline acsawdey

I read that this time the fairing missed by several hundred metres. What happens if it misses by 10 metres and hits the cabin?
My guess: you spend few ten k $ in repairs to boat and write fairing off. Humans inside should be sufficiently protected.

Also note that along with the arms to hold the net, they added a structure behind the cabin that appears to be intended to protect it from a wayward fairing approaching from the rear.

Offline wannamoonbase

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Are they manually controlling the ship?

I assumed they’d eventually end up with computer control and info from a radar to position the ship. 

Building up the SpaceX Robot Navy. 
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!

Offline RocketLover0119

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It is the left to die F9 In flight abort stage 1 that Spacex decided not to use in favor of doing the in flight abort at CCAFS.

From the article written for this mission, what is the rocket core in the background of the picture mentioning the VAFB landing pad construction?

It appears to have two engines? Maybe something previously discussed?

-Splinter
"The Starship has landed"

Offline Paul_G

From the article written for this mission, what is the rocket core in the background of the picture mentioning the VAFB landing pad construction?

It appears to have two engines? Maybe something previously discussed?

-Splinter

I think this was the stage was was going to be used for the inflight Crew Dragon abort. It was built before fuel densification was a thing, and I don't think it is compatible with the PAD GSE as it is configured now, so I don't think it can be launched from any of the SpaceX pads.

Paul

Online abaddon

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It's F9R Dev2, originally intended for flight envelope testing before Dev1 was terminated.

Offline Kabloona

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Are they manually controlling the ship?

I assumed they’d eventually end up with computer control and info from a radar to position the ship. 

Building up the SpaceX Robot Navy.

Probably some type of dynamic positioning system.

https://en.m.wikipedia.org/wiki/Dynamic_positioning

Quote
One of the possibilities is sailing an exact track, useful for cablelay, pipelay, survey and other tasks.

If both the fairing and the ship are pre-programmed to follow the same course, then the remaining variable(s) to be controlled are the ship's speed and position along the pre-programmed course to coincide with the fairing, which maybe is the pilot's input on the throttle.
« Last Edit: 02/23/2018 02:45 pm by Kabloona »

Online gongora

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The fairing recovery vessel should be under manual control unless you really trust the parachutes and wind to land within a couple meters of a set position (which doesn't seem very likely).

Offline fthomassy

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The fairing recovery vessel should be under manual control unless you really trust the parachutes and wind to land within a couple meters of a set position (which doesn't seem very likely).
Seem very likely. Control of the parachute would be much more agile the a ship. Ever seen the Golden Knights land on a target?
gyatm . . . Fern

Offline JonathanD

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Paz launch patch

Translation: "Everything seems impossible until it is accomplished"

Also, I don't remember seeing a SpaceX patch without a clover leaf before, or am I missing it?


edit: better translation

That's a patch from the customer.  The SpaceX PAZ mission patch does indeed have a clover.

https://pbs.twimg.com/media/DWLGNsRX4AEOoYO.jpg

Offline cscott

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The fairing recovery vessel should be under manual control unless you really trust the parachutes and wind to land within a couple meters of a set position (which doesn't seem very likely).
Seem very likely. Control of the parachute would be much more agile the a ship. Ever seen the Golden Knights land on a target?
And yet it missed.

The boat also has a dynamic positioning system which should be able to hold position within a few meters.  And huge thrusters (for its class of ship).

Given that we've seen meter-scale boat positioning accuracy demonstrated on the ASDS, I'm going to go with "the parachute missed" rather than "the boat missed".

Full specs on the boat's dynamic positioning system: http://www.seatranmarine.com/vessels-1/mr-steven

(Elon's tweet suggests to some that the boat is manuveuring to get under the parachute; it could also be read as "the amount of cross-range compensation possible on the chute was not enough given the descent time", ie discussing rates of x/y versus rate of z, with the implication being it was easier to decrease dz than increase dx and dy.)
« Last Edit: 02/23/2018 03:17 pm by cscott »

Offline swervin

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It is the left to die F9 In flight abort stage 1 that Spacex decided not to use in favor of doing the in flight abort at CCAFS.

From the article written for this mission, what is the rocket core in the background of the picture mentioning the VAFB landing pad construction?

It appears to have two engines? Maybe something previously discussed?

-Splinter

Thanks to both of you that answered!

Offline fthomassy

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The fairing recovery vessel should be under manual control unless you really trust the parachutes and wind to land within a couple meters of a set position (which doesn't seem very likely).
Seem very likely. Control of the parachute would be much more agile the a ship. Ever seen the Golden Knights land on a target?
And yet it missed.

The boat also has a dynamic positioning system which should be able to hold position within a few meters.  And huge thrusters (for its class of ship).

Given that we've seen meter-scale boat positioning accuracy demonstrated on the ASDS, I'm going to go with "the parachute missed" rather than "the boat missed".

Full specs on the boat's dynamic positioning system: http://www.seatranmarine.com/vessels-1/mr-steven

(Elon's tweet suggests to some that the boat is manuveuring to get under the parachute; it could also be read as "the amount of cross-range compensation possible on the chute was not enough given the descent time", ie discussing rates of x/y versus rate of z, with the implication being it was easier to decrease dz than increase dx and dy.)
So our opinions agree? The boat hold position and the parachute maneuvers.
gyatm . . . Fern

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