Author Topic: SpaceX Falcon 9 FT - ORBCOMM-2 - Dec. 21, 2015 (Return To Flight) DISCUSSION  (Read 1360654 times)

Online catdlr

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Mr. Scott, I think your right, Space Ship One beat BO, and if you want to take this even further back, the Bell-X2 and all the X=15 flights too.
« Last Edit: 12/23/2015 01:55 am by catdlr »
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Offline joek

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Aren't the unknowns he cites precisely the targets of the experimental research that SpaceX is pursuing? It's reasonable to remain skeptical about the economics of reusability, given that nobody knows at present how much it will cost to make a returned rocket flight ready, how much of a market there will be for used rockets, and how the decreased demand for new materiel will affect the profitability of the company. The issue he raises of loss of performance, however, suggests that he doubts that the modifications to the rocket will achieve what SpaceX has said that they do.

Thanks for the translation assist.

The decrease in manufacturing production requirements is a canard.  This is reminiscent of the broken window fallacy.  The money that would have been put into now unneeded manufacturing will be put to more productive use.

Whether the decrease in performance is material depends on the market.  If SpaceX can satisfy payload needs with reuse, then additional performance above those needs and "loss of capability" is irrelevant. The upcoming SES-9 launch will provide a good indication.

Offline macpacheco

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Classic.  The "it ain't proven yet" line starts at the top.

If it were his own company, he might have worried about the possibility that it might actually work instead of clinging to the hope that it won't.
A Arianespace factory worker has less to worry about in near term from the F9 recovery than SpaceX factory worker. Every recovered booster is one less that SpaceX needs to produce and SpaceX are not known for carrying surplus workers.
I disagree. SpaceX wants to get to 40 launches per year with their Falcons. They currently are at 6. Even with fairly high reuse, they'll need much more rocket stages (upper stages mostly) and about as many rocket engines (when you include occasionally expended boosters plus occasional failed landing/barging plus the eventual retirement due to fatigue and obsolescence). It will take them several years to get to 40 launches, but it will also take several years to get to very high reuse fractions (i.e. 90% of flights reused, and reused for 10 flights). This is also a key point that that Arianespace CEO falters: he fails to grasp the size of SpaceX's launch market ambitions as well as the possibility of continued significant launch market growth (driven in part by lowering launch costs, but some just due to economic growth... though these are interconnected). Reuse will allow SpaceX to do an order of magnitude more launches while keeping their existing manufacturing capabilities well-utilized but also not needing them to be greatly expanded.

And yes, by that time, we'll be talking about BFR and BFS, which WILL need expansion of capability (in terms of size, though not so much numbers except for BFS which will need lots more manufacturing capability). And before SpaceX is really flying BFR/BFS significantly, they'll need to expand manufacturing for their constellation. So yeah, I doubt SpaceX will downsize if reuse works like a charm. Instead, they'll just grow.

C’est une belle réussite technologique dans le cadre d’une mission en orbite basse qui demandait peu de performance au lanceur, libérant ainsi celle exigée par la récupération.

The Ariane Space CEO's first point is that the Orbcomm mission didn't require much from the rocket in terms of performance, thus saving enough fuel for landing. Correct me if I'm wrong, but weren't the modifications to the rocket and the use of super-cooled propellants intended to make feasible GTO missions lifting large communications satellites that also enabled landing?

Mais pour l’équation économique, les choses restent encore très incertaines.


He challenges the economic equation and lists a number of factors.

Perte de performance liée à la récupération, moindre cadence industrielle, coût de remise en état de l’étage, difficulté à convaincre les clients d’utiliser un lanceur d’occasion, incertitudes sur la fiabilité: ce serait une erreur de considérer que la réutilisation est l’alpha et l’oméga de l’innovation de rupture dans le domaine des lanceurs.

1) Loss of performance linked to recovery;
2) Lowered industrial rate, presumably referring to diminished use of productive capacity;
3) Refurbishment costs;
4) Uncertainty regarding the reliability of "used" rockets.

He then concludes that it would be an error to think of reusability as the alpha and omaga of disruptive innovation in the area of rockets.

Aren't the unknowns he cites precisely the targets of the experimental research that SpaceX is pursuing? It's reasonable to remain skeptical about the economics of reusability, given that nobody knows at present how much it will cost to make a returned rocket flight ready, how much of a market there will be for used rockets, and how the decreased demand for new materiel will affect the profitability of the company. The issue he raises of loss of performance, however, suggests that he doubts that the modifications to the rocket will achieve what SpaceX has said that they do.

https://en.wiktionary.org/wiki/pound_the_table

This guy is pounding on the table, as nothing else is really on his side.
He'll never admit that F9R is threatening the economic viability of Ariane 5 already (right now, without reuse), because of the big-little launch model.
He'll never admit that FH even without reuse could be the kiss of death for Ariane.
Add S1 reuse for F9R and FHR, and the whole Ariane model is economically in-viable without billions of Euros in anual subsidies.

I'm really curious what he'll claim when the first FH launch the 3 sticks get recovered...
Looking for companies doing great things for much more than money

Online meekGee

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They'll switch from "It's not proven yet" to "Nobody could have foreseen" + "help us, for the sake of the country".

Classic.  The "it ain't proven yet" line starts at the top.

If it were his own company, he might have worried about the possibility that it might actually work instead of clinging to the hope that it won't.
A Arianespace factory worker has less to worry about in near term from the F9 recovery than SpaceX factory worker. Every recovered booster is one less that SpaceX needs to produce and SpaceX are not known for carrying surplus workers.
I disagree. SpaceX wants to get to 40 launches per year with their Falcons. They currently are at 6. Even with fairly high reuse, they'll need much more rocket stages (upper stages mostly) and about as many rocket engines (when you include occasionally expended boosters plus occasional failed landing/barging plus the eventual retirement due to fatigue and obsolescence). It will take them several years to get to 40 launches, but it will also take several years to get to very high reuse fractions (i.e. 90% of flights reused, and reused for 10 flights). This is also a key point that that Arianespace CEO falters: he fails to grasp the size of SpaceX's launch market ambitions as well as the possibility of continued significant launch market growth (driven in part by lowering launch costs, but some just due to economic growth... though these are interconnected). Reuse will allow SpaceX to do an order of magnitude more launches while keeping their existing manufacturing capabilities well-utilized but also not needing them to be greatly expanded.

And yes, by that time, we'll be talking about BFR and BFS, which WILL need expansion of capability (in terms of size, though not so much numbers except for BFS which will need lots more manufacturing capability). And before SpaceX is really flying BFR/BFS significantly, they'll need to expand manufacturing for their constellation. So yeah, I doubt SpaceX will downsize if reuse works like a charm. Instead, they'll just grow.

C’est une belle réussite technologique dans le cadre d’une mission en orbite basse qui demandait peu de performance au lanceur, libérant ainsi celle exigée par la récupération.

The Ariane Space CEO's first point is that the Orbcomm mission didn't require much from the rocket in terms of performance, thus saving enough fuel for landing. Correct me if I'm wrong, but weren't the modifications to the rocket and the use of super-cooled propellants intended to make feasible GTO missions lifting large communications satellites that also enabled landing?

Mais pour l’équation économique, les choses restent encore très incertaines.


He challenges the economic equation and lists a number of factors.

Perte de performance liée à la récupération, moindre cadence industrielle, coût de remise en état de l’étage, difficulté à convaincre les clients d’utiliser un lanceur d’occasion, incertitudes sur la fiabilité: ce serait une erreur de considérer que la réutilisation est l’alpha et l’oméga de l’innovation de rupture dans le domaine des lanceurs.

1) Loss of performance linked to recovery;
2) Lowered industrial rate, presumably referring to diminished use of productive capacity;
3) Refurbishment costs;
4) Uncertainty regarding the reliability of "used" rockets.

He then concludes that it would be an error to think of reusability as the alpha and omaga of disruptive innovation in the area of rockets.

Aren't the unknowns he cites precisely the targets of the experimental research that SpaceX is pursuing? It's reasonable to remain skeptical about the economics of reusability, given that nobody knows at present how much it will cost to make a returned rocket flight ready, how much of a market there will be for used rockets, and how the decreased demand for new materiel will affect the profitability of the company. The issue he raises of loss of performance, however, suggests that he doubts that the modifications to the rocket will achieve what SpaceX has said that they do.

https://en.wiktionary.org/wiki/pound_the_table

This guy is pounding on the table, as nothing else is really on his side.
He'll never admit that F9R is threatening the economic viability of Ariane 5 already (right now, without reuse), because of the big-little launch model.
He'll never admit that FH even without reuse could be the kiss of death for Ariane.
Add S1 reuse for F9R and FHR, and the whole Ariane model is economically in-viable without billions of Euros in anual subsidies.

I'm really curious what he'll claim when the first FH launch the 3 sticks get recovered...
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Online meekGee

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So do we know how the rocket is processed?

Did they bring the ground mount to the landing pad after the landing?  Or did the crane take the rocket somewhere else?

Are the legs folded in, or removed right there?
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Offline matthewkantar

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The European launcher does have an edge in reliability that will take some time to beat, if SpaceX can beat it. 69 successes in a row is reassuring when you want to put an 8 or 9 billion dollar telescope in orbit.

Matthew

Offline Robotbeat

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The European launcher does have an edge in reliability that will take some time to beat, if SpaceX can beat it. 69 successes in a row is reassuring when you want to put an 8 or 9 billion dollar telescope in orbit.

Matthew
Ariane 5 had SEVERAL major failures in its first flights. Falcon 9 has had 1 out of 20. SpaceX will beat it in time.
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Offline Antilope7724

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The European launcher does have an edge in reliability that will take some time to beat, if SpaceX can beat it. 69 successes in a row is reassuring when you want to put an 8 or 9 billion dollar telescope in orbit.

Matthew

Human crews have various escape systems available on various launchers. Why not a payload escape system for expensive payloads that cost too much to lose?

Offline OxCartMark

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Did they bring the ground mount to the landing pad after the landing?  Or did the crane take the rocket somewhere else?

The 4 piece Falcon mount is only approximately as wide as the body of the rocket, around 12' so there is no way that it could hold the 175' cylinder upright against a wind unless it was anchored to something substantial.  And from the pictures we saw of the foundation being poured in Jacksonville we have circumstantial evidence that the concrete under it is very substantial.  In Jacksonville we saw excavating of the hole and a very large pile of excavated sand in the background.  Presumably that sand volume is the same as the concrete volume and it was voluminous.   The crane took it somewhere.  And in my mind that somewhere is outside of the 2/3 mile diameter cleared area, or at least 2/6 mile (1760 feet) from the center of the circle which is approximately where it landed.  Also, in one of the pictures which was taken from the water it appears that the mount is near the beach (though possibly due to the use of a long lens).

As to the question above on flammability of the working fluid in the landing leg cylinders, its helium which is severely not flammable.

As for the comments by the leader of the European launcher it appears to me that he either doesn't understand what is happening in his industry or does understand but wants to keep everyone happy so that he keeps his job for a while longer than he would if he would if his employers were to panic over what his competition has done.  In either case he wouldn't be my choice to lead the company.
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Offline Kim Keller

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So do we know how the rocket is processed?

Did they bring the ground mount to the landing pad after the landing?  Or did the crane take the rocket somewhere else?

Are the legs folded in, or removed right there?

When I left the cape at 5PM this evening the first stage was still at LZ-1 with a large crane attached to the top of the interstage.

Offline TrevorMonty

The commercial satellite operators want and will support 2- 3 operators, given Ariane's excellent  record Ariane's customers will keep supporting  them. Proton with its patchy reliability  is most likely  to suffer especially  as F9 with reuseability can match Proton for price. A lower price Atlas is more of direct threat  to Ariane 5, both companies  launch on time with exceptionally reliability records.

Online meekGee

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So do we know how the rocket is processed?

Did they bring the ground mount to the landing pad after the landing?  Or did the crane take the rocket somewhere else?

Are the legs folded in, or removed right there?

When I left the cape at 5PM this evening the first stage was still at LZ-1 with a large crane attached to the top of the interstage.

Interesting.

I agree with the oxCartMark's rationale though - on the foundations being somewhere else, a location that is common to all 5 pads.

Someone was wondering upthread why the crane was a big lattice work affair instead of a simple hydraulic telescoping boom.  The answer is there - the tracked lattice cranes can move while carrying load.

So how to reconcile?

Do we know the ground mount is already set up?  If so, maybe there's a foundation poured, with ground-flush anchors that they can pin the above-ground mount to.  And then they wheel them in on demand.

But even so - where on the pad to they put it?  They need to be able to deal with the rocket at any location on the pad...

---

Leg wise - since this stage won't fly, it'll be simpler to take out the legs on the spot instead of re-folding them.  IMO.  But who knows - maybe they want to practice the real thing already.

----

What are they doing at the pad that they can't do later in the hangar?

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Offline matthewkantar

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The European launcher does have an edge in reliability that will take some time to beat, if SpaceX can beat it. 69 successes in a row is reassuring when you want to put an 8 or 9 billion dollar telescope in orbit.

Matthew
Ariane 5 had SEVERAL major failures in its first flights. Falcon 9 has had 1 out of 20. SpaceX will beat it in time.

I am familiar with Ariane's teething problems. If Spacex is flawless from here out, it will still be several years before they have 69 successes in a row. The tension between constant innovation and reliability is real.

Matthew

Offline Lars-J

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The European launcher does have an edge in reliability that will take some time to beat, if SpaceX can beat it. 69 successes in a row is reassuring when you want to put an 8 or 9 billion dollar telescope in orbit.

Matthew
Ariane 5 had SEVERAL major failures in its first flights. Falcon 9 has had 1 out of 20. SpaceX will beat it in time.

I am familiar with Ariane's teething problems. If Spacex is flawless from here out, it will still be several years before they have 69 successes in a row. The tension between constant innovation and reliability is real.

Sure... But Ariane's problems are also real. Reliability isn't as important for commercial customers as you might think, otherwise ULA and Arianespace would have complete dominance.

Yes, they have a certain captive market (EU govt launches), but should they start losing commercial customers, they will be forced to raise costs significantly for their other launches - OR make significant cuts. Cuts that could have negative impacts on reliability. They need to figure out a way to lower costs ahead of the curve, or they will find that Ariane 6 is too little too late.

Online Chris_Pi

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meekGee - There's an environmental assesment (http://www.patrick.af.mil/shared/media/document/AFD-141107-004.pdf) that has crane paths and a trailer/pedestal area marked on pages 23/24. It looks to me like they just pick it up off the pad with the crane and drive over there to set it down on the stand. Once you have to move the whole rocket upright at all a few thousand feet probably isn't much more work than a few hundred.

Online Comga

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meekGee - There's an environmental assesment (http://www.patrick.af.mil/shared/media/document/AFD-141107-004.pdf) that has crane paths and a trailer/pedestal area marked on pages 23/24. It looks to me like they just pick it up off the pad with the crane and drive over there to set it down on the stand. Once you have to move the whole rocket upright at all a few thousand feet probably isn't much more work than a few hundred.

And that's the answer I was looking for, the "Trailer/Pedestal Area".
Good work, Chris_Pi!
Thanks
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

Offline mulp

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Ariane's problem is not Falcon 9 with reuse, but simply Falcon 9 and then Falcon Heavy.

Falcon 9 has already put price pressure on the industry based on subcontractors to satisfy political interests in the 50s, 60s, 70s. While lots of consolidation and mergers have reduced the friction cost of scattered development and production, it is hard to reorganize to benefit from technology. In the 60s, thousands of people were needed simply to track blue prints and check things. More to translate prints to parts casting and machining details.

SpaceX has used computer and software technology from the start and have certainly gone as directly as possible to master design to component machining code or welding instructions. I'm sure the steps are manual, but the coordinates and paths automatic.

I'm sure that for too many of the competitors, the part design is converted from one cad format to another to create a new part cad file hat is converted into machining code.  It took Boeing decades to integrate, but it contracted and partnered with software vendors so it's suppliers would be able to respond quickly.  Along comes SpaceX starting almost from scratch building on the decades of work Boeing required. (GM was pushing this in parallel with visions of transforming all the divisions of GM that started out as separate car companies with their own way of doing business.)

SpaceX product strategy is classic computer-hardware standard modules reused and reused in different configurations. This contrasts with pretty much all other design where engineers see standard modules as being suboptimal. In other rocket companies, there are multiple unique designs that are optimized for specific purposes.

So, if Falcon Heavy is delivers on hopes with say only 5% unique fit up of Falcon 9 parts, improvements to Falcon 9 flow to Falcon Heavy with low cost and delay (not zero, but low).

Competitors will be required to focus their minds on competing with SpaceX instead of competing between who gets the work, France or Germany, Alabama or Texas.

And they will need to either find the niche where SpaceX can't serve because it's outside the window of current standard modular construction, or be better than SpaceX in modular design.

As for Ariane, they have planned to end Ariane 5 and replace with 6, so, they must be seriously considering alternatives.

And even Falcon Heavy is not going to match Saturn V, which is from the 60s.

I've lived long enough to not instantly reject the idea that the total industry launch market is ten times larger by 2020. And at that point, Saturn V class launches at today's pace of total industry launch will something customers are willing to put deposits on for 2025. For what I have no idea. But in the 60s, the jet plane traffic of today was beyond comprehension, and certainly not imagined as stuffing people in like sardines.

Offline NASAsupporter9

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The first stage appears to have buckled right above the octoweb.

You can see this most clearly in the 10 second video Elon Musk tweeted as "Live video from LZ-1," but you can also see it 33:35 into the entire launch video. However, the lighting is deceptive in both video.

The buckling probably happened upon contact with the ground, the relight for landing, or max-Q upon re-entry. The landing seemed pretty gentle, but the landing relight would have had the highest structural loads from the thrust do the the reduced propellant mass. However if max-Q occurred during the re-entry burn, the re-entry loads could have exceeded the landing burn. The thrust and aerodynamic drag would be summed to produce the force the structure was subjected to.

It all depends on how high they were during the re-entry burn, how rarified the atmosphere was, and how fast they were going. I'm not sure how SpaceX have the octoweb seated in the aluminum core, but clearly the access holes they usually place at the base of the aluminum core are a weak spot (if the ocotweb supports the aluminum core that low). The buckling is why I don't think they will re-fly the stage, which violates their previously stated plans.

How could they strengthen the base of the stage? Thicken the aluminum? Add internal struts? Create vertically spread internal attachment points for the Octoweb or front bulkhead?

Can anyone make out if the buckling had occured prior to landing form the helo video?




Online guckyfan

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It may look like bucking in a few frames. But I am sure it is only the uneven soot. They have declared after landing they will use the stage for wet dress rehearsal and hot fire tests on LC-39A after landing. No way they would do that with a buckled tank.

Online Steven Pietrobon

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Please indicate where you see the buckling in this capture, because I can't see anything wrong.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

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