Talk:SpaceX launch vehicles

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I'm thinking the main section of the air-launch rocket should be in the main SpaceX article with this page having a small reference to it, because while the rocket may be based on the Falcon series it isn't officially part of the Falcon family, let alone have any SpaceX branding. 69.38.128.246 (talk) 21:20, 15 December 2011 (UTC)[reply]

I do not disagree actually. I am not entirely sure that even this wikipedia article is necessary, as almost all of the current "rocket family" all derivations of the Falcon 9: but that is for another debate at another time.--Abebenjoe (talk) 22:33, 15 December 2011 (UTC)[reply]

I think the article is necessary because it's about the rockets from mostly a technical standpoint while the other article should be reduced to spacex as a business, including some details about the falcons but also, dragon, company history, missions, nasa/stratolaunch contracts, etc TMV943 (talk) 02:46, 16 December 2011 (UTC)[reply]

I, too, don't believe that the Falcon (rocket family) article ought to be deleted, or merged. Why? It is a (fairly newly created) article that documents a notable set of 21st century private rocket development projects.

I believe the—perhaps poorly executed—intent of the editor who created this article was to remove a good bit of the detail of the SpaceX rocket family of Falcon rockets from the main SpaceX article. I think this is probably a good intent, and worthwhile goal. However, when this article was created, nearly all the rocket info was totally deleted from the main SpaceX article, not leaving even well-written prose summaries, and without any prior discussion on the SpaceX Talk page; so I reverted the deletion in the SpaceX article. Probably still needs clean up, reduction, and copy editing over there. Cheers. N2e (talk) 06:13, 16 December 2011 (UTC)[reply]

Gosh, thanks for being subtle :(. Actually the two things I removed was the chart (which is really all or nothing, but I'll let you decide when it's time) and the future development, which may have been more questionable. TMV943 (talk) 05:04, 17 December 2011 (UTC)[reply]

The article currently claims that the Stratolauch "Air-launched rocket" that SpaceX is developing will "For the human-rated version, no exact details have been released on what spacecraft will be used; however, it will use a feathered-return,{{dubious|date=December 2011}} low-drag reentry system similar to [[Scaled Composites]]'s sub-orbital [[SpaceShipOne]] spacecraft.<ref name=avw20111213/>"

This claim is not supported by the referenced source. That Aviation Week article (13 Dec 2011) says this: "Rutan said the human-rated Falcon system will fly the “feathered” low-drag re-entry profile he used for SpaceShipOne." Flying a re-entry profile that may be low-drag, is not the same as utilizing a feathered return system on the human-carrying space capsule.

In short, we would need more direct evidence that Stratolaunch is intending something other than a capsule for this "air-launched rocket" before we should make this assertion in Wikipedia. So I will intend to remove the unsupported claim. N2e (talk) 14:48, 21 February 2012 (UTC)[reply]

There are a number of photos released in the past few days of the Grasshopper (rocket) VTVL test vehicle, here. I would think that someone who is Wiki-photo-wise (which is definitely not me) could figure out how we could use one of these photos under a fair use rationale. I'll add a {{reqphoto}} tag. Cheers. N2e (talk) 03:57, 13 July 2012 (UTC)[reply]

Considering that the article as a whole has a large number of available-to-use free photos, I personally couldn't justify uploading a non-free image for a single section. Perhaps someone near McGregor could...get near and snap a pic? — Huntster (t @ c) 05:36, 13 July 2012 (UTC)[reply]

Thanks, Huntster. I see your point on the overall quantity of photos in the article. But of course, that fails to provide a photo of this particular VTVL rocket.

Well, I guess the logic for obtaining a photo for this particular notable new rocket that is under funded development will work better after some editor separates the mere article section into its own article, which will no doubt happen in the coming months or years. Cheers. N2e (talk) 13:46, 20 July 2012 (UTC)[reply]

 Done User:Craigboy has helpfully uploaded a Creative Commons licensed photo from the Flickr fotstream of Steve Jurvetson. Good work! Removed the reqphoto tag. N2e (talk) 05:17, 16 September 2012 (UTC)[reply]

Some editor has moved the Falcon 1e to cancelled, but I've not seen any cited source that supports that. Rather, the sources I've seen seem to indicate that the Falcon 1e was either "late in development" or "developed" at the time that SpaceX chose to discontinue offering Falcon 1e flights on the market (ostensibly at least in part because its order book was low/limited) and concentrate company operational resources on the Falcon 9. Does anyone have a source that the Falcon 1e is, indeed, "cancelled"? If not, I'll soon remove the rocket from the "Cancelled" section of the article. Cheers. N2e (talk) 04:49, 26 July 2012 (UTC)[reply]

The Falon 1e was designed, but no Falcon 1e was launched or even built before the program was discontinued. That makes it a paper rocket, which justifies the statement "cancelled". At least that was my train of thought when I saw what had been done;). — Gopher65_talk 14:46, 26 July 2012 (UTC)[reply]

Well, thanks for offering your logic up. Appreciate that. But I believe that it was a serious, funded development program, that was well down the path of significant money having been spent for both development and also for verification and validation, and was already scheduled for the new model to come into the production line on a certain mission, when SpaceX decided that they would halt taking orders for all Falcon 1 launches (both F1 and F1e) and move the payloads they had manifested to Falcon 9. Either way, it is not dependent on my thoughts ("...I believe...") nor your thoughts ("my train of thought...". We just need a source that says Falcon 1e was actually "cancelled" as opposed to merely SpaceX decided to stop scheduling launches on a launcher that was well down the development path. Failing that, we should not show the launcher as "cancelled" in the Wikipedia article. N2e (talk) 21:56, 29 July 2012 (UTC)[reply]

The Falcon 1e basically went from being ready for payload orders to being wiped from the site much like the different Falcon 9 blocks. So I doubt it was just a concept rocket but without a launch there really hasn't been much tracking its development TMV943 (talk) 00:44, 30 July 2012 (UTC)[reply]

Since no source supporting the "cancelled" claim has been provided in the past week, I have moved the Falcon 1e material back into the Falcon 1 section of the article, per discussion above. If a source surfaces later that indicates SpaceX has, indeed, cancelled the entire Falcon 1e program, we can update the article then. N2e (talk) 22:13, 1 August 2012 (UTC)[reply]

The Falcon 1e will never fly. Still it is listed in the comparison table. Remove that column? Kcauwert (talk) 23:00, 26 April 2015 (UTC)[reply]

SpaceX has announced development of a new Super-heavy launch vehicle, utilizing a new SpaceX-developed LOX/LH2 rocket engine called the "MCT". Little is known about it at present beyond very rough thrust and total payload mass to low-Earth orbit. I have found no name at all for the new SHLift launch vehicle. I had originally added a new section to this article with a summary and a source.

However, as another editor (User:TMV943) has pointed out, nothing in the sources to date says that this new launch vehicle will be known by the designator 'Falcon', so it would seem the new launch vehicle probably does not belong in this article at this time. (Ditto for the MCT, which has not been identified as a 'Merlin' engine; so probably does not belong in the Merlin series article either.) This could be opened for discussion. But to this point, I tend to agree with the editor who removed the MCT section, text I had previously added, and placed it in the SpaceX main article. Cheers. N2e (talk) 13:17, 21 October 2012 (UTC)[reply]

"Little is known about it at present beyond very rough thrust and total payload mass to low-Earth orbit."

We don't even know that really as the statements referring to the new engine and the payload mass of a SHLift rocket were two different announcements and the new engine may be part of a different vehicle design to the original concept. ChiZeroOne (talk) 14:07, 21 October 2012 (UTC)[reply]

I totally agree. The published reports to date do not indicate whether the engines will be a member of the Merlin family (seems unlikely since the fuel is LOX/LH2 rather than LOX/RP1), or whether the upper stage LOX/LH2 engine is even the Raptor second stage engine concept that SpaceX has occasionally spoken out about since 2009. Also, as User:TMV943 pointed out, they may or may not be "Falcon" rockets. So as of now, having nothing about them is appropriate in this article. N2e (talk) 14:15, 4 November 2012 (UTC)[reply]

The one caveat is that both of these (Merlin 2 and MCT) are intended to be used in "Super-heavy lift vehicles". It might be that there are two engine development programs, with the Merlin 2 intended for a range of lift capability under that of the MCT. However, there is far to litte information to really tell. My gut feeling is that the Merlin 2 is being replaced with MCT. In any event, it is perhaps better with one section/page on all SpaceX "Super-heavy lift" engine developments. After all, the Falcon X and HeavyX etc were merely conceptual "brainstorming ideas", just a "bunch of ideas for discussion," and not financed SpaceX projects as clarified by Elon (and the current text reads). That is, I agree that the MCT should not be included here, but in a sense, neihter should the Falcon X. They are both just heavy-lift concepts based on proposed new engines. FalconX can stil be included here, but the bulk of the information on "Super-heavy lift" designs and engines could be on a new page. SC2Buran (talk) 21:31, 12 November 2012 (UTC)[reply]

They have the Falcon name, so they get a mention on the Falcon rocket family page TMV943 (talk) 03:16, 13 November 2012 (UTC)[reply]

I have attempted to cover all SpaceX engines, whether RP-1, or Methane, or hypegolic, in the SpaceX rocket engine family article. Other editors are welcome to help to help improve that article. (Note that there is, as of December 2012, no mention of the MCT in that article, as various sources have explicitly indicated that MCT is not a a rocket engine, even though several media sources reported that when the "MCT" descriptor was first used by SpaceX earlier in the fall of 2012. Even though there is no MCT rocket engine at all, the article page MCT (rocket engine) is a redirect, and one that just survived an RfD discussion over the past couple of weeks.) There is, however, a mention of the VERY LARGE ROCKET ENGINE that SpaceX is developing in the SpaceX rocket engine family article, without giving it any name at all, since SpaceX has not named it yet. — Cheers. N2e (talk) 21:18, 24 December 2012 (UTC)[reply]

The table claims that the initial thrust of the F9 is 3400 kn, without any citation adjacent to the claim, but with a grouping of three sources given under the table that are purporting to support ALL of the claims in the table.

The one source that seems most likely for the F9 initial thrust claim, is the Dec 2011 archive (one of the three sources underneath the table) for the Falcon 9. This source reports that the "a total thrust on liftoff of just over 1.1 Million lbs-f." 1.1 million lbf is NOT 3400 kn, rather 1.1 M lbf is ^{[convert: unit mismatch]} (1,100,000 lbf); or 9500 kN. A rather large error.

I have not fixed that error yet, but it is illustrative of a larger problem: attempting to source an entire table full of specific claims—claims that will inevitably change over time in the emergent world of Wikipedia—from one or more sources at the bottom of a table, is problematic. Even if the entire table is correctly sourced at some point in time, it inevitably won't be at a later time as my efforts to confirm the F9 data showed today. Definitely will need much more work. Cheers. N2e (talk) 19:37, 24 December 2012 (UTC)[reply]

1.1M lbf is actually about 4900 kN. I'm not going to comment on the sourcing issue but at least mathematically it seems to makes sense; a Merlin 1C has about 350kN Sea level thrust, 350kN*9 = 3150kN. The 4900 kN could be for the 1.1 TMV943 (talk) 21:02, 24 December 2012 (UTC)[reply]

Thanks for the comment, TMC943. That number is still a rather large difference from what is in the article. Please take a look at what the convert template does with the 1,100,000 lbf above; it seems to come out with 9500 kN. Do you think the Wikipedia convert template has a calculation error in it? N2e (talk) 21:07, 24 December 2012 (UTC)[reply]

Testing convert:1,100,000 pounds-force (^{[convert: unit mismatch]}), using: {{convert|1100000|lbf|kn}}. Yeah, there's a bug in there somewhere. Are we sure we're talking pounds force and not something like foot-pounds? 1.1 million pounds-force = ~4900 kilo-newtons (Google convert claims 4850 or so). There are 4.448 newtons in 1 pound (linky). If we're talking foot-pounds though, that's a unit of energy , and isn't directly translatable into newtons. Dunno why we'd be talking foot-pounds, I'm just trying to figure out the discrepancy. — Gopher65_talk 03:06, 25 December 2012 (UTC)[reply]

Gopher65: We are definitely talking units of force here, that is to say, either Newtons or pounds-force (lbf). We are not talking foot-pounds, which is a unit of torque, not force. Cheers. N2e (talk) 04:55, 25 December 2012 (UTC)[reply]

I have started a discussion over at Template_talk:Convert#Potential_conversion_error:_lbf_to_Newtons, asking for some help from a Convert template guru. N2e (talk) 04:55, 25 December 2012 (UTC)[reply]

See my reply there (use kN for kilonewtons). Johnuniq (talk) 07:36, 25 December 2012 (UTC)[reply]

Okay, thanks Johnuniq. It was my editor error in the use of the {{convert}} template. "kn" is knots. "kN" is kilonewtons.

So, we see, testing 1,100,000 pounds-force (4,900 kN), using: {{convert|1100000|lbf|kN}} gives us 4900 kN. Cool.

With a few other features turned on, we get 1.1 M lbf is 4,900 kN. — N2e (talk) 12:41, 25 December 2012 (UTC)[reply]

 Done — the table is fixed now, and I found a way to get the convert template to output only the converted number, and not the units, so now it looks right at home in the table cell. N2e (talk) 21:12, 26 December 2012 (UTC)[reply]

For quite some time, the "Launch vehicle comparisons" table in the article has purported that it was sourced from three sources via a footnote at the bottom of the table. The three sources were two from 2011, and one from 2007.

On 24 Dec 2012, I did a careful update of the Falcon 9 claims in that table. MOST of the table entries were incorrect, and the numbers that had been in the article were not, in general, supported by those three sources. I have cleaned up the Falcon 9 v 1.0 column (on 24 Dec) and individually cited the claims that can be supported by a known source. Today (25 Dec), I've done the same for the Falcon 9 v1.1 column.

NET: these three (old) sources clearly DO NOT source the ENTIRE table. Leaving them in the article just encourages sloppy editing when many editors, and many readers, improperly assume that (old) sources at the bottom of a table source everything in a table. While this is possible, it generally quickly degenerates in the emergent world of Wikipedia where subsequent editors may change the numbers, without updating the sources.

I will plan to remove those archaic/outdated sources from the footnote at the bottom of the table at a later time. They may, however, be useful for supporting particular individual claims in the table. Cheers. N2e (talk) 14:31, 25 December 2012 (UTC)[reply]

N2e's recent editing has highlighted what I've long seen as a problem with these articles: the "price per kilogram" section of the table is nothing more than guesswork derived from the maximum payload and the published price ranges. Even if Wikipedia editors were in a position to do original research like that (we're not), those two values ranges are both approximate. The max payload depends greatly on the exact orbital altitude and the inclination of the orbit (merely saying "to LEO" doesn't tell the reader much), while the price of the launch depends on mission requirements, size of contract, etc. They are not set values, and thus we can't use them to compute a reliable price per kilogram. Even computing a minimum price per kilogram is problematic, because we don't know what the "normal" price per launch and normal max launch masses are going to turn out to be (both will differ from their theoretic min values).

I'd like to remove 3 price per kilo rows from the table. I don't want a vote, but instead I'd like to discuss this and see if anyone can justify the existence of those rows beyond the obvious "it's fun speculation". — Gopher65_talk 20:13, 26 December 2012 (UTC)[reply]

• Support the proposal to remove the three "price per kilogram" rows in the table. They are unsourced (and therefore likely {{original research}} and are notoriously difficult to be compared in a table anyway, since if sources are found for some claims, they are typically done at different times by different authors using different cost methodologies, and so are simply not comparable in any meaningful way. N2e (talk) 13:32, 29 December 2012 (UTC)[reply]

 Done — Gopher65_talk 00:08, 2 April 2013 (UTC)[reply]

Good work. Glad to see that done! Now there are many more places where these non-comparable and only partially complete price/kg comparisons have been inserted into launcher-related articles. See, for example, Comparison of orbital launch systems. N2e (talk) 00:27, 2 April 2013 (UTC)[reply]

The sections for Grasshopper and reusable launching system are a bit redundant. What's more they may not be placed correctly. Grasshopper is only intended as a testbed so in a way it can be considered active in its mission rather than "under development". However, I wouldn't put it on the active list since it's more of a related rocket than an actual Falcon. Instead I'd take the reusable rocket section and put it in "under development" since it is under development in that Grasshopper is part of that goal, and add Grasshopper as a sub-section to that TMV943 (talk) 06:45, 10 March 2013 (UTC)[reply]

Good point. SpaceX seems to be doing a lot of work on the reusable launching system, only one part of which is the Grasshopper version 1 (short tank, low-altitude) rocket. There is the v1.1 Grasshopper (long-tank, higher-altitude, fold-up legs, supersonic-flight capable) rocket, and with announcement in only the past week, a fairly extensive very high-altitude, very fast (Mach 10 (12,300 km/h; 7,610 mph)) booster-return and over-water simulated "landing" testing they are going to be doing on all future F9 v1.1 rockets, beginning this June. I like the idea that Grasshopper is probably a subsection of the reusable development and test program that SpaceX is doing. Cheers. N2e (talk) 05:53, 30 March 2013 (UTC)[reply]

The SpaceX reusable rocket launching system is now described in an article of its own. Grasshopper v1.0, and the under construction Grasshopper v1.1, vehicles are a couple of components of that very active experimental technology rocket vehicle development program. As well, the fly-back tests of the Falcon 9 v1.1 first stages that will begin at mid-year 2013 is also a part of the the SpaceX reusable rocket launching system program. Take a look at that article, and then feel free to help improve the effort to describe the two things in context in that article, or on that new article's Talk page. Cheers. N2e (talk) 04:58, 1 April 2013 (UTC)[reply]

I've added a bit of information to begin to clarify/summarize the distinctions between the (now retired) Falcon 9 v1.0 and the currently-in-service Falcon 9 v1.1. Even though we will want to leave most of the detail on those two rockets in their respective articles, there is probably a bit more summary info to add, and definitely more cleanup of this article to do, to present that story more encyclopedically. I'll try to get back here and do it sometime, but if anyone else in interested in copyediting and organizing to improve the Falcon rocket family article, that would be fine by me. Cheers. N2e (talk) 04:35, 17 October 2013 (UTC)[reply]

Great additional information about the v1.1, thanks. Karl (talk) 14:41, 17 October 2013 (UTC)[reply]

I'm curious as to what other people think about this article's inclusion of the Merlin 2 and other related material (like the Falcon X). It seems to me that these projects have been superceded by the MCT and the Raptor family of engines. We haven't heard anything about a Merlin 2 engine in a long time, so I think maybe we should start culling outdated references to that engine and its "just brainstorming" rockets. — Gopher65_talk 14:32, 11 January 2014 (UTC)[reply]

Remove Merlin 2, it doesn't exist, and it was mentioned only officially once.--Abebenjoe (talk) 01:00, 15 February 2015 (UTC)[reply]

Yes, remove it. See my comment below, in the next section. N2e (talk) 05:10, 15 February 2015 (UTC)[reply]

K, I've removed the Merlin 2 content at least. I left the Raptor stuff that was in that section, but it's not correct. According to the most recent Reddit AMA by Elon Musk (as well as an MIT talk he gave), the Raptor will only be 1/4 as powerful (and 1/5th as large) as previously estimated by the SpaceX fanclub (which was where the 1 to 1.5 million figure came from), because that is the "sweet spot" for the thrust-to-weight ratio with the design they're working on. — Gopher65_talk 23:41, 15 February 2015 (UTC)[reply]

The section dealing with Future proposals is a total mess, and is completely out-of-date. I will be heavily revising it, as those concepts are not "future", but are "historic" what-ifs, and should not be in this article.--Abebenjoe (talk) 01:02, 15 February 2015 (UTC)[reply]

I concur. All the material on "Merlin 2", "Falcon X", and "Falcon XX" were merely conceptual powerpoint slides presented at a conference, and which were quickly walked back by Musk and the official company a few days/weeks later. Moreover, what has since come to past, and is now actual development work, is not very much like any of that conceptual stuff. I'd be fine if the material was removed, or summarized with a sentence or two, either one. N2e (talk) 05:09, 15 February 2015 (UTC)[reply]

Would this image be usable on Wikipedia? It's a highly encyclopaedic image created by reddit users /u/ethan829 and /u/dante80 source, essentially by compositing public renders made by SpaceX. All SpaceX photos are released under public domain licences, I wonder if that includes these renders? Anxietycello (talk) 20:45, 30 October 2015 (UTC)[reply]

The article has some strangenesses now. The v1.1 section starts talking about 2005 (which is clearly and more correctly either the F5 or the F9 v1.0). The "under development" Falcon 9R, a term used extensively by SpaceX for while during development (along with other related terms like reusable Falcon 9 and Falcon 9 reusable etc.) is pretty clearly not still under development as is currently stated. But that material should also not just be deleted completely and lose the History of the family of rockets and its development. F9R and reusable Falcon 9 lingo was clearly a chapter in the development of this launch vehicle family. (I just reverted a complete and large deletion of that material.)

But clearly, the article needs some considerable work to get it in better order. Anyone have ideas? Anyone want to help? Let's discuss a few meta-concepts here and see if we might develop consensus on some top-level organisation and then get some editing underway. Cheers. N2e (talk) 00:19, 24 July 2016 (UTC)[reply]

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The planned BFR launch vehicle is not part of the Falcon line. For example, it would use the Raptor, not the Merlin engines. Also, BFR does not stand for Big Falcon Rocket. This section should be removed, and possible replaced with a reference to a page on the BFR or a note that the Falcon line will be discontinued to facilitate development and production of the BFR.

Fcrary (talk) 18:53, 1 October 2017 (UTC)[reply]

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There is no single source for this but a bit of research shows that there is no mention of attaining Mars orbit and in any case is unfeasible until April/May at the earliest.

The logical conclusion is that the second stage will send the payload into a Hohmann transfer orbit which will pass near to the PATH of the orbit of Mars (not Mars itself which will arrive around that point about 3 months later) and then without a further burn will just stay in that precessing, elliptical orbit, presumably coming back round the the sun with its periapsis at the distance of the Earth's orbit and then back to its apoapsis at the distance of the Mars orbit.

There is no info on the following, but to avoid close passes to either planet, you would have to assume that they would tilt axis of the plane of the orbit slightly off of the planetary plane, making collision or interference with satellites etc, impossible in the future, and allow it to continue safely in its orbit for "billions of years".

I think it would be good to clear up this common misconception.

Here's a ref that backs this up: ^[1]

Calscot (talk) 16:54, 3 January 2018 (UTC) — Preceding unsigned comment added by Calscot (talk • contribs) 16:39, 3 January 2018 (UTC)[reply]

Therefore we can add this rocket to the retired spacex vehicles — Preceding unsigned comment added by AkaSoftBanana (talk • contribs) 13:48, 29 March 2018 (UTC)[reply]

No, in that the current Block 4 (which are no longer being manufactured, but a few remain to be flown and/or reflown) and forthcoming Block 5 are just enhancements of the Full Thrust version. Rosbif73 (talk) 13:05, 5 April 2018 (UTC)[reply]

I should note that we can't automatically apply this discussion to other pages. Red Slash 17:58, 16 September 2019 (UTC)[reply]

I'm sure we can apply the rationale used in this page for the renaming of at least the category, started a discussion Wikipedia:Categories for discussion/Log/2019 September 16#Category:Falcon (rocket family). OkayKenji ^{(talk page)} 20:25, 16 September 2019 (UTC)[reply]

@PhilipTerryGraham: I have restored the title "SpaceX launch vehicles" stipulated in the RM outcome. If you'd like to further switch to "Launch vehicles of SpaceX", you should open a followup RM. — JFG ^talk 04:03, 19 September 2019 (UTC)[reply]

@JFG: Patently unfair. There was no rationale to move it to that particular title, meanwhile I provided a rationale for "Launch vehicles of SpaceX". Surely the burden therefore is not on me to open a discussion on it. There needs to be some reason the article should be titled that way. – PhilipTerryGraham (talk · articles · reviews) 06:42, 19 September 2019 (UTC)[reply]

Three participants explicitly favored "SpaceX launch vehicles" over the initially-proposed title "Rockets of SpaceX", and the closer chose this accordingly. You then changed it unilaterally to "Launch vehicles of SpaceX", which was never mentioned in the discussion. Even if you provided a rationale for your change, that doesn't trump RM consensus. Thanks for opening a new RM to test acceptance of your proposal. — JFG ^talk 07:57, 19 September 2019 (UTC)[reply]

@JFG: "...which was never mentioned in the discussion" – you've just further proven my belief that nobody actually reads the opening proposals of move discussions. Half of the opening is dedicated to describing why the "[subject] of [company]" format was put forward – "The proposal has been modified from "SpaceX rockets", as the name format implies a brand or subdivision of SpaceX, where as "Rockets of SpaceX" would be consistent with similar articles such as History of SpaceX as a sub-article of SpaceX". Please stop distorting reality to fit your narrative and recognise that the only thing close to a rationale in that discussion was that the "[company][subject]" format was that it "could also be good title", which is, and I cannot for the life of me stress this enough, not a rationale. Consensus is not a blind vote; "Consensus on Wikipedia does not mean unanimity (which is ideal but not always achievable), neither is it the result of a vote. Decision making and reaching consensus involve an effort to incorporate all editors' legitimate concerns". Nobody attempted to argue against the original proposed format, and thus that logically means there was no problem with it. We're supposed to come up with a reason as to why one thing is better than the other. – PhilipTerryGraham (talk · articles · reviews) 10:07, 19 September 2019 (UTC)[reply]

Look, I have read your rationale before !voting, and you cannot presume that other participants somehow did not read it properly. Had there been straight support for your proposed title, that would have been readily apparent to the uninvolved closer. Instead, as often happens in RM discussions, several people settled on an alternate title. You may or may not like the outcome, but that's no reason to make a further move out of process. Re: ...which was never mentioned in the discussion, that's a fact. The title you suggested was "Rockets of SpaceX", and the title you now prefer "Launch vehicles of SpaceX" was indeed never mentioned until your bold move. — JFG ^talk 10:48, 19 September 2019 (UTC)[reply]

I check pages listed in Category:Pages with incorrect ref formatting to try to fix reference errors. One of the things I do is look for content for orphaned references in wikilinked articles. I have found content for some of SpaceX launch vehicles's orphans, the problem is that I found more than one version. I can't determine which (if any) is correct for this article, so I am asking for a sentient editor to look it over and copy the correct ref content into this article.

Reference named "ars20200305":

• From SpaceX Starship: berger, Eric (5 March 2020). "Inside Elon Musk's plan to build one Starship a week—and settle Mars". Ars Technica. Retrieved 6 March 2020. Musk tackles the hardest engineering problems first. For Mars, there will be so many logistical things to make it all work, from power on the surface to scratching out a living to adapting to its extreme climate. But Musk believes that the initial, hardest step is building a reusable, orbital Starship to get people and tons of stuff to Mars. So he is focused on that.
• From SpaceX South Texas Launch Site: berger, Eric (5 March 2020). "Inside Elon Musk's plan to build one Starship a week—and settle Mars". Ars Technica. Retrieved 5 March 2020.

I apologize if any of the above are effectively identical; I am just a simple computer program, so I can't determine whether minor differences are significant or not. AnomieBOT⚡ 13:11, 13 March 2020 (UTC)[reply]

It looks like the same article. OkayKenji ^{(talk page)} 13:46, 13 March 2020 (UTC)[reply]

Fixed. OkayKenji ^{(talk page)} 06:08, 16 March 2020 (UTC)[reply]

The falcon 1 isnt partially reusable, and not even the source claims it is Fehér Zsigmond-03 (talk) 11:00, 10 April 2024 (UTC)[reply]

The Falcon 1 article tells us that [t]he first stage was originally planned to return by parachute to a water landing and be recovered for reuse and cites sources. This is presumably the basis for the "partially reusable" wording in this article. If you're feeling WP:BOLD, you could always change the text to say "designed to be partially reusable" or similar. Rosbif73 (talk) 12:21, 10 April 2024 (UTC)[reply]