Talk:Delta IV: Difference between revisions
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== History == |
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Why is there nothing about the history of Delta IV? "The Delta IV entered the space launch market when global capacity was already much higher than demand" tells us nothing. Is it embarrassment that the only US space rocket is 60 years old? I suggest adding a brief history going back to the origins of Delta.[[User:Royalcourtier|Royalcourtier]] ([[User talk:Royalcourtier|talk]]) 02:51, 6 December 2014 (UTC) |
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Corrected some incorrect data about the launch sites and spacecraft. -- [[User:Nick L.|Nick L.]] |
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* [https://web.archive.org/web/19990117064504/http://www.boeing.com/defense-space/space/delta/delta4/delta4.htm The U.S. Air Force announces the procurement of Boeing Delta IV launches] covers it : |
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"Delta IV/Evolved Expendable Launch Vehicle Program On Oct. 16, 1998, the U.S. Air Force announced the procurement of 19 Boeing Delta IV launches for the Evolved Expendable Launch Vehicle (EELV) program valued at $1.38 billion. |
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"This initial launch services contract covers small, medium and heavy payload class launches from 2002 to 2006. It splits 28 missions in a dual-source procurement designed to encourage greater contractor investment and competition in the U.S. space launch industry, and to decrease the Air Force's overall development cost. |
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"The Air Force also entered into a $500 million agreement with Boeing, supplementing development of the Delta IV family of launch vehicles for meeting all Air Force EELV requirements. |
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"The Boeing Delta IV/Evolved Expendable Launch Vehicle Program (EELV) is a multi-year U.S. Air Force effort aimed at reducing space launch costs by more than 25 percent. To meet these requirements, Boeing is offering the Delta IV family of vehicles. The family includes five launch vehicles: Medium, Heavy, and three variants of the Medium vehicle, known as Medium-plus, which have been introduced to meet the needs of the commercial market. |
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"Program Timing |
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"The EELV program development and procurement cycle began in 1995. During the first phase, four competitors completed a 15-month contract to validate low-cost concepts. In December 1996, two contractors were selected to participate in the second phase, known as the Pre-Engineering, Manufacturing and Development (Pre-EMD) phase, a firm, fixed-price 17-month contract worth $60 million for each company." |
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- [[User:Rod57|Rod57]] ([[User talk:Rod57|talk]]) 03:48, 5 January 2024 (UTC) |
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== Primary Units of Measure == |
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I'm not sure if this can be used for anything, but there's a nice photo of the Delta IV's second-stage here: http://mediaarchive.ksc.nasa.gov/detail.cfm?mediaid=24253 --[[User:NeuronExMachina|NeuronExMachina]] 02:15, 19 Dec 2004 (UTC) |
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[[WP:UNITS]] says "In non-scientific articles relating to the United States, the primary units are US customary" applies since this is a US product. Some exceptions the Delta IV rocket that I can think of are payload mass and the 4 m and 5 m diameters. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 18:05, 18 March 2015 (UTC) |
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:Why should payload be an exception? All other modern LVs [[Atlas V]] [[Antares (rocket)|Antares]] [[Falcon 9 v1.1]] [[Delta II]] [[Pegasus (rocket)|Pegasus]] etc use SI primary units. If US customary is the primary unit, then the entire article and all the other ones should be changed to reflect that, including payload. Modern US spaceflight articles have been using SI without issue for a long time (this one has for over a decade), why crack the UNITS whip randomly? UNITS is a guideline, there are always exceptions, and common sense says these articles should remain consistent. -[[User:Anythingcouldhappen|'''''<span style="color:blue">A</span>''''']]([[User talk:Anythingcouldhappen|'''''<span style="color:green">Ch</span>''''']]) 18:57, 18 March 2015 (UTC) |
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:: [[WP:Other stuff exists]]. I am just stating what the MoS tells us to do. You can try invoking [[WP:IAR]] if you want. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 19:52, 18 March 2015 (UTC) |
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:::Then why is payload an exception? If MOS is to be rigorously applied, payload should be in US units. So MOS always has exceptions; modern US spaceflight articles have consistently used SI and this article should follow that convention. [[User:Anythingcouldhappen|'''''<span style="color:blue">A</span>''''']]([[User talk:Anythingcouldhappen|'''''<span style="color:green">Ch</span>''''']]) 20:45, 18 March 2015 (UTC) |
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:I agree; since the vehicle is currently active, SI is the appropriate primary unit, and there's no good reason to treat the payload differently (perhaps if the US manufacturer were stuck using English engineering units, with international payload customers, but that's not the case here.) Keeping one convention consistent in this article is certainly least confusing. [[User:JustinTime55|JustinTime55]] ([[User talk:JustinTime55|talk]]) 19:43, 18 March 2015 (UTC) |
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I read that Boeing and Mitsubishi were developing a more powerful upper stage engine called MB-60 for use on the Delta IV. However, I have not seen any updates for several years. Does anyone know if this is still being developed?--[[User:Todd Kloos|Todd Kloos]] 04:23, 24 Dec 2004 (UTC) |
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:: I don't get why being active make SI primary? The DIV vehicles were designed primarily in US units as most US companies do. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 19:52, 18 March 2015 (UTC) |
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:::I certainly agree with your comment about US industry. I guess the two determining factors in whether SI primary makes sense, are (I have to confess ignorance about the specifics of the Delta IV): |
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* How "private" is the rocket, i.e. does it fall under NASA's metric directive? |
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* How dependent is it on the Delta legacy vehicle? [[User:JustinTime55|JustinTime55]] ([[User talk:JustinTime55|talk]]) 20:07, 18 March 2015 (UTC) |
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:::I don't think it can be asserted that DIV was designed primarily in US units, and it's moot anyway - the issue is consistency with other modern US spaceflight articles. [[User:Anythingcouldhappen|'''''<span style="color:blue">A</span>''''']]([[User talk:Anythingcouldhappen|'''''<span style="color:green">Ch</span>''''']]) 20:45, 18 March 2015 (UTC) |
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:::* If consistency trumps everything, then I'm wasting my time here. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 20:51, 18 March 2015 (UTC) |
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::::Surely consistency is an important factor. If UNITS is enforced here, it should be equally applied to all US spaceflight articles, should it not? [[User:Anythingcouldhappen|'''''<span style="color:blue">A</span>''''']]([[User talk:Anythingcouldhappen|'''''<span style="color:green">Ch</span>''''']]) 21:08, 18 March 2015 (UTC) |
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::::* I think it should, but US spaceflight articles covers a lot of articles and not something I want to get into, hence I mentioned WP:Other stuff exists above. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 21:12, 18 March 2015 (UTC) |
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:::::Therefore, since this article used SI primary for over a decade and was consistent with other US spaceflight articles, does applying UNITS here improve the article? [[User:Anythingcouldhappen|'''''<span style="color:blue">A</span>''''']]([[User talk:Anythingcouldhappen|'''''<span style="color:green">Ch</span>''''']]) 21:21, 18 March 2015 (UTC) |
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Spacecraft articles overlap science and technology. I think that the consistency that matters is to inform the reader regardless of their nationality. Being that the metric International System is, well, international, I feel that the primary unit should be metric followed by a conversion to Imperial. As the WP article stands now, the primary for height is feet and the primary for diameter is meter (without conversion). Whatever you decide, do it consistently. Cheers, [[User:BatteryIncluded|BatteryIncluded]] ([[User talk:BatteryIncluded|talk]]) 21:16, 18 March 2015 (UTC) |
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== Capitalization of class names == |
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:The article is still inconsistent, with the primary unit for vehicle mass being lbm and the primary unit for payload mass being kg, also without conversion. [[User:Anythingcouldhappen|'''''<span style="color:blue">A</span>''''']]([[User talk:Anythingcouldhappen|'''''<span style="color:green">Ch</span>''''']]) 08:18, 19 March 2015 (UTC) |
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::My two cents: the primary units in the article are best if consistently in one system of measure. I too take the approach on these things that for modern spaceflight-related vehicles and spacecraft, then SI units as primary and the more esoteric local units as secondary/parenthetical makes the most sense for the English Wikipedia's very large international readership. So for me, since Delta IV is a modern launch vehicle, not one of the early history of tech type articles from 1960s, then SI (non-SI) is best. [[User:N2e|N2e]] ([[User talk:N2e|talk]]) 12:33, 19 March 2015 (UTC) |
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The Boeing site (from the link on the main page) refers to each variant with a capitalized name (i.e. Medium or Heavy as opposed to medium or heavy) whenever they are reffered to. Because of this, and if no one objects, I'd like to go through and change all of the references to this format. I think it can be succesfully argued that these are all proper nouns as used, rather than simply adjectives. --[[User:Icelight|Icelight]] 29 June 2005 15:25 (UTC) |
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== |
== Delta IV Medium == |
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Is this configuration already retired? <!-- Template:Unsigned IP --><small class="autosigned">— Preceding [[Wikipedia:Signatures|unsigned]] comment added by [[Special:Contributions/94.220.12.243|94.220.12.243]] ([[User talk:94.220.12.243#top|talk]]) 08:38, 3 January 2017 (UTC)</small> <!--Autosigned by SineBot--> |
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: ULA is retiring the the Delta IV Medium versions; the comparable Atlas V versions will be used instead since they cost less. Here's an [http://www.defensenews.com/story/defense/air-space/space/2015/03/15/ula-delta-iv-retire-rd180-russia-spacex/70231994/ article] about that. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 15:31, 4 January 2017 (UTC) |
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If nobody has a problem with it, I would like to add some info about the upcoming [[GOES]]-N launch on a Delta IV tomorrow. [[User:Nick L.|Nick L.]] 15:57, 28 July 2005 (UTC) |
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:Launch delayed ;-) --[[User:Bricktop|Bricktop]] 22:15, 28 July 2005 (UTC) |
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== Separate Delta IV and Delta Heavy Launches Page? == |
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''The first launch of a valuable payload aboard the Delta IV Heavy is scheduled for fall 2005'' -- does this article need an update? [[User:Ojw|Ojw]] 20:44, 20 January 2006 (UTC) |
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Most of the other rockets have separate launches pages, as that information is separate from the vehicles themselves. Should we move that information to a new page? [[User:UnknownM1|UnknownM1]] ([[User talk:UnknownM1|talk]]) 06:18, 19 February 2018 (UTC) |
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I just noticed there is a weird kind of hybrid page of multiple different rockets, separated by decades, under the "Delta" wing. It is very confusing and sort of unhelpful. It seems that the whole page needs reform or rework. [[User:UnknownM1|UnknownM1]] ([[User talk:UnknownM1|talk]]) 06:20, 19 February 2018 (UTC) |
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: The GOES-N flight is currently scheduled for Feburary 6, 2006. Might as well wait until the launch to do an update. [http://www.osd.noaa.gov/GOES/goes-launch.htm Linky]. [[User:Jbanes|Jbanes]] 21:51, 3 February 2006 (UTC) |
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:*Those were taken care of by others today. I corrected the wording on DSP-23 and added NROL-25 & 26 based on launch manifest[http://www.spaceflightnow.com/tracking/index.html] (forgot to login). -[[User:Fnlayson|Finlayson]] 03:43, 25 May 2006 (UTC) |
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: Note that the Delta Heavy IS still a Delta IV rocket variant. [[User:Fnlayson|-Finlayson]] ([[User talk:Fnlayson|talk]]) 13:42, 19 February 2018 (UTC) |
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::No I am aware. I think it is a List of Thor and Delta Rocket Launches, but the article layout itself is confusing and there shouldn't be the same information on multiple pages. [[User:UnknownM1|UnknownM1]] ([[User talk:UnknownM1|talk]]) 15:50, 19 February 2018 (UTC) |
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::: OK, I just wanted to clarify about keeping them together. Splitting up the launches by rocket model seems clearer than by decade as done with Thor and Delta launches now, imo. [[User:Fnlayson|-Finlayson]] ([[User talk:Fnlayson|talk]]) 16:16, 19 February 2018 (UTC) |
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:Yes, launches should be grouped by major evolution, i.e. Delta "alpha", Delta "numeric", Delta II + III, Delta IV, Delta IV Heavy. As a rule of thumb, if a rocket version has a dedicated article, it probably deserves a dedicated list of launches. — [[User:JFG|JFG]] <sup>[[User talk:JFG|talk]]</sup> 17:38, 19 February 2018 (UTC) |
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== |
== Number of Launches (in Infobox) == |
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The Delta IV rocket has launched 39 times, and it even says that later in the article. However, in the infobox it still says it's only launched 37 times. Can that please be updated? [[User:SnowballEffect|SnowballEffect]] ([[User talk:SnowballEffect|talk]]) 23:23, 12 May 2019 (UTC) |
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: The Infobox has been updated now. You could have just updated them or started on it yourself. [[User:Fnlayson|-Fnlayson]] ([[User talk:Fnlayson|talk]]) 00:21, 13 May 2019 (UTC) |
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The page had stated that Delta IVs launched from the "same site" as the Apollo 1 fire and Apollo 7, however, those launches were from SLC-34, just next door to 37B. The [[Apollo_1]] and [[Apollo_7]] pages confirm this. I can also vouch from personal experience, having stood inside the launch ring on SLC-34 and seen a loaded booster from the parking lot at SLC-37. (sadly, that launch got scrubbed and I missed it. :() |
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==Partial success== |
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I'm new here so someone who knows better please fix the laugable "partial sucesess" thing re the dec 2004 launch. Eliminating POV, that means failure. Wiki is not a public relations firm is it. <small>—''The preceding [[Wikipedia:Sign your posts on talk pages|unsigned]] comment was added by'' [[User:65.188.193.14|65.188.193.14]] ([[User talk:65.188.193.14|talk]] • [[Special:Contributions/65.188.193.14|contribs]]) {{{2|}}}.</small><!--Inserted with Template:Unsigned--> |
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:I don't see where calling something a "partial success" is POV. Doing any activity is rarely black and white. Launching rockets is no different. Had the payload been lost that would be a failure. This was a demonstration launch. Most of the goals of the demonstration were met. There was a failure in terms of the early fuel out indication, but the test payload did make it into orbit. For me at least that fits as partial. |
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:On one other note, please sign your comments on talk pages with four tildes (<nowiki>~~~~</nowiki>) to let others know who said what. Thanks. --[[User:StuffOfInterest|StuffOfInterest]] 13:09, 20 January 2006 (UTC) |
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::I would like to throw in a few cents. Partial success is used in numerous places in the industry to describe notable accidents that didn't cause a complete mission loss of the launch vehicle. You see it in the standard text ''International Reference Guide to Space Launch Systems'', Iaskowitz, Hopkins, and Hopkins. You see it in other industry reference sites etc. If you don't like its use that's fine, but there's a difference between it being marketing fluff by Boeing and it being the standard way the industry talks about such accidents. Having the article consistent with industry practice is perfectly reasonable. [[User:Georgewilliamherbert|Georgewilliamherbert]] 22:36, 20 January 2006 (UTC) |
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:::If the mission were carrying a real satellite, then yes, it would be a failure. However, in light of what the mission was - a TEST mission, it is a partial success. This is why the USAF decided to fly a test mission, to make sure everything works. Not only did this mission prove out many aspects of the Heavy variant, it accomplished what a test flight is meant to do - find problems so that they can be fixed before something important ends up in a low orbit. [[User:Nick L.|Nick L.]] 06:37, 21 January 2006 (UTC) |
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== RS-68 details-move to own page? == |
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I thought that this article had too much of a focus on the RS-68, so I removed some of the information from the article (i.e the channel-wall construction, etc...) and plan on moving it to the [[RS-68 (rocket engine)|RS-68]] article. Any opinions or objections? [[User:Nick L.|Nick L.]] 15:19, 21 July 2006 (UTC) |
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* Good move. The Delta article doesn't need every detail on the RS-68 engine. - [[User:Fnlayson|Fnlayson]] 15:53, 21 July 2006 (UTC) |
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== Standard article titles? == |
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Randomly discovered that while this article is called [[Delta IV rocket]], while [[Delta II rocket]] is a redirect to [[Delta II]]. Maybe something more standard? [[User:-b|-b]] 19:33, 20 August 2006 (UTC) |
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* The titles probably should include rocket to be consistent. [[Delta rocket]] needs rocket in the name to prevent confusion with other things. -[[User:Fnlayson|Fnlayson]] 20:46, 20 August 2006 (UTC) |
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* '''Oppose''' There are no valid grounds to disambiguate Delta II or Delta IV. <font color="#002222">'''GW_Simulations'''</font><sub>''[[User:GW Simulations||User Page]]'' | ''[[User talk:GW_Simulations|Talk]] ''|'' [[Special:Contributions/GW_Simulations|Contribs]]'' | ''[[User:GW Simulations/Chess|Chess]]'' | ''[[Special:Emailuser/GW_Simulations|E-mail]]''</sub> 22:59, 21 August 2006 (UTC) |
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==Requested move== |
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<div class="boilerplate" style="background-color: #efe; margin: 2em 0 0 0; padding: 0 10px 0 10px; border: 1px dotted #aaa;"><!-- Template:polltop --> |
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:''The following discussion is an archived debate of the {{{type|proposal}}}. <font color="red">'''Please do not modify it.'''</font> Subsequent comments should be made in a new section on the talk page. No further edits should be made to this section. '' |
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{{{result|The result of the debate was}}} |
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[[Delta IV rocket]] → [[Delta IV]] – Unnecessary disambiguation <font color="#002222">'''GW_Simulations'''</font><sub>''[[User:GW Simulations||User Page]]'' | ''[[User talk:GW_Simulations|Talk]] ''|'' [[Special:Contributions/GW_Simulations|Contribs]]'' | ''[[User:GW Simulations/Chess|Chess]]'' | ''[[Special:Emailuser/GW_Simulations|E-mail]]''</sub> 18:49, 21 August 2006 (UTC) |
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===Survey=== |
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Add "* Support" or "* Oppose" followed by an optional one-sentence explanation, then sign your opinion with <nowiki>~~~~</nowiki> |
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*'''Oppose.''' [[Delta rocket]] and [[Delta III rocket]] both contain "rocket" in the title as well - this article's title is consistent with that, if anything, [[Delta II]] should be changed. [[User:Nick L.|Nick L.]] 19:09, 21 August 2006 (UTC) |
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::These contain "rocket" because there is a valid disambiguation - pages already exist at [[Delta]] and [[Delta III]]. In this case, [[Delta IV]] simply redirects here, so it is not a valid disambiguation. --<font color="#002222">'''GW_Simulations'''</font><sub>''[[User:GW Simulations||User Page]]'' | ''[[User talk:GW_Simulations|Talk]] ''|'' [[Special:Contributions/GW_Simulations|Contribs]]'' | ''[[User:GW Simulations/Chess|Chess]]'' | ''[[Special:Emailuser/GW_Simulations|E-mail]]''</sub> 19:12, 21 August 2006 (UTC) |
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:::<s>Ah, I see - I didn't understand the request properly. Strike my vote.</s> [[User:Nick L.|Nick L.]] 19:35, 21 August 2006 (UTC) |
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::::After further consideration, I am unstriking my vote. [[User:Nick L.|Nick L.]] 00:55, 27 August 2006 (UTC) |
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* '''Oppose'''. The Delta article has rocket in the name to avoid disambiguity. The other Delta vehicle articles should be consistent with that. -[[User:Fnlayson|Fnlayson]] 22:46, 21 August 2006 (UTC) |
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::But there is nothing here to avoid ambiguity with. --<font color="#116655">'''GW_Simulations'''<sub>[[User:GW Simulations|<font color="#000000">User Page</font>]] | [[User talk:GW_Simulations|<font color="#000000">Talk</font>]]</sub></font> 11:30, 26 August 2006 (UTC) |
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::*That's already been stated. The name change will make little difference with Redirects anyway. -[[User:Fnlayson|Fnlayson]] 16:12, 26 August 2006 (UTC) |
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* '''Support'''. There is no disambiguation page named "Delta IV". [[User:Bigtop|<font color="blue">Big</font>]][[User talk:Bigtop|'''<font color="gray">top</font>''']] 16:57, 22 August 2006 (UTC) |
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* '''Support'''. [[User:-b|-b]] 14:49, 23 August 2006 (UTC) |
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* '''Oppose.''' Better to keep it consistent with [[Delta III rocket]], which can't change. [[User:Andrewa|Andrewa]] 02:55, 27 August 2006 (UTC) |
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===Discussion=== |
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*Closing RM after a week.. doesn't look like consensus to move. Leaving here for now. -[[User:Goldom|Goldom]] [[User_talk:Goldom|‽‽‽]] [[Special:Contributions/Goldom|⁂]] 03:58, 27 August 2006 (UTC) |
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:''The above discussion is preserved as an archive of the debate. <font color="red">'''Please do not modify it.'''</font> Subsequent comments should be made in a new section on this talk page. No further edits should be made to this section.</div><!-- Template:pollbottom --> |
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* I know it's too late to vote, but the reasons for not moving above are not very convincing. Disambiguation should be done with parenthetic remarks to make it clear what the name of the subject of the article is (the part that is not in parentheses). Making "rocket" part of the title implies that "rocket" is part of the name of the rocket. --[[User:Serge Issakov|Serge]] 23:34, 1 September 2006 (UTC) |
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== Infoboxes == |
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Looks like a fair amount of the infomation in the 2 infoboxes is common for both like 1st and 2nd stage engines. One infobox with extra lines for the different vehicle type would cover things. Anybody see a problem with this? -[[User:Fnlayson|Fnlayson]] 17:09, 23 September 2006 (UTC) |
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:Done. --<font color="#116655">'''GW_Simulations'''<sub>[[User:GW Simulations|<font color="#000000">User Page</font>]] | [[User talk:GW_Simulations|<font color="#000000">Talk</font>]]</sub></font> 19:10, 28 September 2006 (UTC) |
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:: Looks good, thanks. -[[User:Fnlayson|Fnlayson]] 19:33, 28 September 2006 (UTC) |
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== Splitting the Delta IV article == |
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*The proposal is to split away the past & planned launches in to a seperate article to clear away large amounts of technicla data.--[[User:Aces lead|aceslead]] 20:52, 22 October 2006 (UTC) |
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===Survey=== |
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Add "* Support" or "* Oppose" followed by an optional one-sentence explanation, then sign your opinion with <nowiki>~~~~</nowiki> |
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*'''SUPPORT''' The article has gotten to long with technical facts about past and planed launches. That information should be split off into a seperate article with all that technical data of past, present and future launches.--[[User:Aces lead|aceslead]] 20:29, 22 October 2006 (UTC) |
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*'''Oppose''' A seperate launch page is not needed yet. The launch list and launch tables have redundant info. Cull info down or remove tables. -[[User:Fnlayson|Fnlayson]] 08:08, 23 October 2006 (UTC) |
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===Discussion=== |
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* Perhaps ALL the "Delta launches" for [[Delta II]], [[Delta III]], & [[Delta IV]].--[[User:Aces lead|aceslead]] 20:29, 22 October 2006 (UTC) |
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*Funny you should mention it. I have been working (offline) on such an article for the last few days. I have finished the 0100, 1000 and 6000, and have most of the 2000 and 7000, along with some of the 3000. It should be online soon. Although I have no intention of changing the content of these articles when it is created, I suppose that it would be an option.--<font color="#116655">'''GW_Simulations'''<sub>[[User:GW Simulations|<font color="#000000">User Page</font>]] | [[User talk:GW_Simulations|<font color="#000000">Talk</font>]]</sub></font> 08:42, 23 October 2006 (UTC) |
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== Delta IV Small? == |
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I don't see why this is listed in the Infobox. It was proposed at one stage in the development, but that's it. If someone wants to mention this in the article that's fine btu it shouldn't be in the infobox. -[[User:Fnlayson|Fnlayson]] 15:17, 4 November 2006 (UTC) |
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* The removal of the DIV Small is already explained at the bottom of the variant section. Overlap with the Delta II is one reason, I beleive. -[[User:Fnlayson|Fnlayson]] 00:27, 5 November 2006 (UTC) |
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== To restart an old debate... == |
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A while ago we debated moving [[Delta IV rocket]] to [[Delta IV]]. This was rejected for consistency with [[Delta III rocket]], which is so named to disambiguate from [[Delta III class submarine]]. [[Delta III class submarine]] is now proposed to be merged into [[Delta class submarine]]. If this goes ahead, then iw would be possible to move both rocket articles ([[Delta IV rocket]] -> [[Delta IV]] and [[Delta III rocket]] -> [[Delta III]]). This addresses the objections raised before. --<font color="#116655">'''GW_Simulations'''<sub>[[User:GW Simulations|<font color="#000000">User Page</font>]] | [[User talk:GW_Simulations|<font color="#000000">Talk</font>]]</sub></font> 17:18, 4 November 2006 (UTC) |
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* Wasn't this already coverd by these proposals efforts? [[Wikipedia talk:Naming conventions (rockets)]] [[Wikipedia:WikiProject Launch vehicles#Naming conventions]] -[[User:Fnlayson|Fnlayson]] 00:37, 5 November 2006 (UTC) |
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**[[WP:ICBM]] fell through due to lack of interest, and the [[WP:LV]] proposal only covers what to do IF disambiguation is required, not whether it should be. For the record, I have merged the submarine articles that I mentioned above. --<font color="#116655">'''GW_Simulations'''<sub>[[User:GW Simulations|<font color="#000000">User Page</font>]] | [[User talk:GW_Simulations|<font color="#000000">Talk</font>]]</sub></font> 14:03, 12 November 2006 (UTC) |
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== Launch Cost == |
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The article says Delta IV launches are priced between $140-170 million. However this appears to only cover the cost of the Delta IV Medium's; astronautix.com states that the price of a Delta IV Heavy launch was "..revised by the USAF in November 2004 to $ 254 million." Perhaps a better breakdown of cost would be appropriate as follows (2004 dollars from astronautix.com, probably higher in 2006 accounting for inflation): |
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Medium $140 million |
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Medium+(4.2) $140 million |
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Medium+(5.2) $150 million |
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Medium+(5.4) $160 million |
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Heavy $254 million. |
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Thoughts? [[User:Subzero788|Subzero788]] | [[User talk:Subzero788|talk]] 09:10, 5 November 2006 (UTC) |
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* Seems reasonable. Replace the periods with comma like (4,2) etc. though. The cost for the Heavy and other types that haven't launched (M+5,2 & M+5,4) will change (generally down) after a few launches. But that a topic for the future. -[[User:Fnlayson|Fnlayson]] 16:40, 14 November 2006 (UTC) |
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== Renaming to disambiguate (again) == |
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There are or were seven "Delta IV" (Project 667BDRM, Delfin) submarines. I understand it has been discussed a zillion times, but would anyone strenuosly object if I rename this article to [[Delta IV (rocket)]] or [[Delta IV (launch system)]]? Can't we then easily [[pipe-trick]] the times we want articles to read, [[Delta IV (whatever)|Delta IV]]? [[User:Sdsds|Sdsds]] 08:15, 16 April 2007 (UTC) |
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:I have made these into redirects. You can now user the pipe trick without having to rename the article. -- [[User:Petri Krohn|Petri Krohn]] 13:05, 16 April 2007 (UTC) |
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== Aerial Photo == |
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The picture of "A unique aerial view of NROL-22 launch from SLC-6" Is obviously a picture of models as evidenced by the wooden toy trucks in the lower right corner of said photo. |
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Recommend that its caption be changed or the photo removed. ~~ChrisCTurner 02:28, 31 May 2008 (UTC) |
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: Garbage. That's not models. It was NROL-22 launch from Vandenberg. Click on the image link and find this [http://www.af.mil/news/story_media.asp?storyID=123022521 Air Force photos page]. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 02:42, 31 May 2008 (UTC) |
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Thanks for the link. Just thought it looked like models and the object in the lower right corner still looks a lot like a wooden toy truck but I'll concede the point. <small>—Preceding [[Wikipedia:Signatures|unsigned]] comment added by [[User:Chriscturner|Chriscturner]] ([[User talk:Chriscturner|talk]] • [[Special:Contributions/Chriscturner|contribs]]) 04:14, 6 June 2008 (UTC)</small><!-- Template:Unsigned --> <!--Autosigned by SineBot--> |
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== Q on Throttling == |
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The article says "Typically, the RS-68 runs at 102% rated thrust for the first few minutes of flight, and then throttles down to 58% rated thrust before main engine cutoff. On the Heavy variant, the core CBC's engine throttles down to 58% rated thrust around 50 seconds after liftoff, while the strap-on CBCs remain at 102%. This allows the core CBC to conserve propellant and burn longer." I assume under either scenario (with or without strap-ons), there is some advantage to throttling back, perhaps having to do with the fact that as you burn fuel and oxidizer, the vehicle masses less and less, and that throttling back maintains some kind of ideal thrust-to-mass ratio (although I don't understand why you wouldn't gradually throttle back as fuel burns, instead of dropping in one step from 102% to 58%). A side effect of that (mentioned in the quote) would be burning longer, although again it's not immediately obvious to me why lower thrust for a longer time is better than higher thrust for a shorter time (it's not the gradually lower air drag, is it?). Is there a discussion of this somewhere in wikipedia? And if so, could this para link to it? [[User:Mcswell|Mcswell]] ([[User talk:Mcswell|talk]]) 19:02, 28 June 2009 (UTC) |
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: On the Heavy DIV, the 3 CBCs hold the same amount of fuel, so the center one is trottled back so it can burn after the strap-on CBCs are spent and jettisoned. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 20:07, 28 June 2009 (UTC) |
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: I believe that the thrust is scaled back to limit the maximum acceleration (proportional to thrust/mass) that the payload or upper stage needs to endure, thereby allowing the upper stages to have reduced structural weight. I also gather that the RS-68 engine is only capable of either 102% or 58% thrust levels. That is, it is not continuously variable. As for the reason why it is not continuously variable, that I don't know. Increased development costs, perhaps? --[[Special:Contributions/71.214.211.224|71.214.211.224]] ([[User talk:71.214.211.224|talk]]) 17:41, 10 October 2010 (UTC) |
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as you say, many boosters, cut throttle to avoid Over-G'ing the upper stage or payload.--[[Special:Contributions/71.178.199.89|71.178.199.89]] ([[User talk:71.178.199.89|talk]]) 17:05, 13 April 2011 (UTC) |
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== updated data, launch capacities == |
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hello the launch capacities mentioned in this article are old and wrong and can be cleaned up from this new official 2009 source: http://www.ulalaunch.com/docs/product_sheet/DeltaIVProductCardFinal.pdf <span style="font-size: smaller;" class="autosigned">—Preceding [[Wikipedia:Signatures|unsigned]] comment added by [[Special:Contributions/76.11.124.147|76.11.124.147]] ([[User talk:76.11.124.147|talk]]) 14:37, 24 July 2009 (UTC)</span><!-- Template:UnsignedIP --> <!--Autosigned by SineBot--> |
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== Ares V info obsolete == |
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The paragraph about using the RS-68 engine in the Ares V rocket (in the Future variants section) seems to be obsolete after the termination of this program. However, my knowledge is too limited to fix this properly. [[User:Sandeman684|Sandeman684]] ([[User talk:Sandeman684|talk]]) 10:20, 13 March 2011 (UTC) |
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: True, but the RS-68 was considered for use on the [[Ares V]]. I believe the RS-68 and Shuttle's SSME were both considered for that. I adjusted the wording to clarify this and use past tense. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 16:24, 13 March 2011 (UTC) |
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== History == |
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Why is there nothing about the history of Delta IV? "The Delta IV entered the space launch market when global capacity was already much higher than demand" tells us nothing. Is it embarrassment that the only US space rocket is 60 years old? I suggest adding a brief history going back to the origins of Delta.[[User:Royalcourtier|Royalcourtier]] ([[User talk:Royalcourtier|talk]]) 02:51, 6 December 2014 (UTC) |
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== Primary Units of Measure == |
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[[WP:UNITS]] says "In non-scientific articles relating to the United States, the primary units are US customary" applies since this is a US product. Some exceptions the Delta IV rocket that I can think of are payload mass and the 4 m and 5 m diameters. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 18:05, 18 March 2015 (UTC) |
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:Why should payload be an exception? All other modern LVs [[Atlas V]] [[Antares (rocket)|Antares]] [[Falcon 9 v1.1]] [[Delta II]] [[Pegasus (rocket)|Pegasus]] etc use SI primary units. If US customary is the primary unit, then the entire article and all the other ones should be changed to reflect that, including payload. Modern US spaceflight articles have been using SI without issue for a long time (this one has for over a decade), why crack the UNITS whip randomly? UNITS is a guideline, there are always exceptions, and common sense says these articles should remain consistent. -[[User:Anythingcouldhappen|'''''<span style="color:blue">A</span>''''']]([[User talk:Anythingcouldhappen|'''''<span style="color:green">Ch</span>''''']]) 18:57, 18 March 2015 (UTC) |
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:: [[WP:Other stuff exists]]. I am just stating what the MoS tells us to do. You can try invoking [[WP:IAR]] if you want. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 19:52, 18 March 2015 (UTC) |
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:I agree; since the vehicle is currently active, SI is the appropriate primary unit, and there's no good reason to treat the payload differently (perhaps if the US manufacturer were stuck using English engineering units, with international payload customers, but that's not the case here.) Keeping one convention consistent in this article is certainly least confusing. [[User:JustinTime55|JustinTime55]] ([[User talk:JustinTime55|talk]]) 19:43, 18 March 2015 (UTC) |
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:: I don't get why being active make SI primary? The DIV vehicles were designed primarily in US units as most US companies do. -[[User:Fnlayson|Fnlayson]] ([[User talk:Fnlayson|talk]]) 19:52, 18 March 2015 (UTC) |
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History
[edit]Why is there nothing about the history of Delta IV? "The Delta IV entered the space launch market when global capacity was already much higher than demand" tells us nothing. Is it embarrassment that the only US space rocket is 60 years old? I suggest adding a brief history going back to the origins of Delta.Royalcourtier (talk) 02:51, 6 December 2014 (UTC)
"Delta IV/Evolved Expendable Launch Vehicle Program On Oct. 16, 1998, the U.S. Air Force announced the procurement of 19 Boeing Delta IV launches for the Evolved Expendable Launch Vehicle (EELV) program valued at $1.38 billion. - "This initial launch services contract covers small, medium and heavy payload class launches from 2002 to 2006. It splits 28 missions in a dual-source procurement designed to encourage greater contractor investment and competition in the U.S. space launch industry, and to decrease the Air Force's overall development cost. - "The Air Force also entered into a $500 million agreement with Boeing, supplementing development of the Delta IV family of launch vehicles for meeting all Air Force EELV requirements. - "The Boeing Delta IV/Evolved Expendable Launch Vehicle Program (EELV) is a multi-year U.S. Air Force effort aimed at reducing space launch costs by more than 25 percent. To meet these requirements, Boeing is offering the Delta IV family of vehicles. The family includes five launch vehicles: Medium, Heavy, and three variants of the Medium vehicle, known as Medium-plus, which have been introduced to meet the needs of the commercial market. - "Program Timing "The EELV program development and procurement cycle began in 1995. During the first phase, four competitors completed a 15-month contract to validate low-cost concepts. In December 1996, two contractors were selected to participate in the second phase, known as the Pre-Engineering, Manufacturing and Development (Pre-EMD) phase, a firm, fixed-price 17-month contract worth $60 million for each company." - Rod57 (talk) 03:48, 5 January 2024 (UTC)
Primary Units of Measure
[edit]WP:UNITS says "In non-scientific articles relating to the United States, the primary units are US customary" applies since this is a US product. Some exceptions the Delta IV rocket that I can think of are payload mass and the 4 m and 5 m diameters. -Fnlayson (talk) 18:05, 18 March 2015 (UTC)
- Why should payload be an exception? All other modern LVs Atlas V Antares Falcon 9 v1.1 Delta II Pegasus etc use SI primary units. If US customary is the primary unit, then the entire article and all the other ones should be changed to reflect that, including payload. Modern US spaceflight articles have been using SI without issue for a long time (this one has for over a decade), why crack the UNITS whip randomly? UNITS is a guideline, there are always exceptions, and common sense says these articles should remain consistent. -A(Ch) 18:57, 18 March 2015 (UTC)
- WP:Other stuff exists. I am just stating what the MoS tells us to do. You can try invoking WP:IAR if you want. -Fnlayson (talk) 19:52, 18 March 2015 (UTC)
- Then why is payload an exception? If MOS is to be rigorously applied, payload should be in US units. So MOS always has exceptions; modern US spaceflight articles have consistently used SI and this article should follow that convention. A(Ch) 20:45, 18 March 2015 (UTC)
- WP:Other stuff exists. I am just stating what the MoS tells us to do. You can try invoking WP:IAR if you want. -Fnlayson (talk) 19:52, 18 March 2015 (UTC)
- I agree; since the vehicle is currently active, SI is the appropriate primary unit, and there's no good reason to treat the payload differently (perhaps if the US manufacturer were stuck using English engineering units, with international payload customers, but that's not the case here.) Keeping one convention consistent in this article is certainly least confusing. JustinTime55 (talk) 19:43, 18 March 2015 (UTC)
- I don't get why being active make SI primary? The DIV vehicles were designed primarily in US units as most US companies do. -Fnlayson (talk) 19:52, 18 March 2015 (UTC)
- I certainly agree with your comment about US industry. I guess the two determining factors in whether SI primary makes sense, are (I have to confess ignorance about the specifics of the Delta IV):
- I don't get why being active make SI primary? The DIV vehicles were designed primarily in US units as most US companies do. -Fnlayson (talk) 19:52, 18 March 2015 (UTC)
- How "private" is the rocket, i.e. does it fall under NASA's metric directive?
- How dependent is it on the Delta legacy vehicle? JustinTime55 (talk) 20:07, 18 March 2015 (UTC)
- I don't think it can be asserted that DIV was designed primarily in US units, and it's moot anyway - the issue is consistency with other modern US spaceflight articles. A(Ch) 20:45, 18 March 2015 (UTC)
- If consistency trumps everything, then I'm wasting my time here. -Fnlayson (talk) 20:51, 18 March 2015 (UTC)
- Surely consistency is an important factor. If UNITS is enforced here, it should be equally applied to all US spaceflight articles, should it not? A(Ch) 21:08, 18 March 2015 (UTC)
- I think it should, but US spaceflight articles covers a lot of articles and not something I want to get into, hence I mentioned WP:Other stuff exists above. -Fnlayson (talk) 21:12, 18 March 2015 (UTC)
- Therefore, since this article used SI primary for over a decade and was consistent with other US spaceflight articles, does applying UNITS here improve the article? A(Ch) 21:21, 18 March 2015 (UTC)
- I don't think it can be asserted that DIV was designed primarily in US units, and it's moot anyway - the issue is consistency with other modern US spaceflight articles. A(Ch) 20:45, 18 March 2015 (UTC)
Spacecraft articles overlap science and technology. I think that the consistency that matters is to inform the reader regardless of their nationality. Being that the metric International System is, well, international, I feel that the primary unit should be metric followed by a conversion to Imperial. As the WP article stands now, the primary for height is feet and the primary for diameter is meter (without conversion). Whatever you decide, do it consistently. Cheers, BatteryIncluded (talk) 21:16, 18 March 2015 (UTC)
- The article is still inconsistent, with the primary unit for vehicle mass being lbm and the primary unit for payload mass being kg, also without conversion. A(Ch) 08:18, 19 March 2015 (UTC)
- My two cents: the primary units in the article are best if consistently in one system of measure. I too take the approach on these things that for modern spaceflight-related vehicles and spacecraft, then SI units as primary and the more esoteric local units as secondary/parenthetical makes the most sense for the English Wikipedia's very large international readership. So for me, since Delta IV is a modern launch vehicle, not one of the early history of tech type articles from 1960s, then SI (non-SI) is best. N2e (talk) 12:33, 19 March 2015 (UTC)
Delta IV Medium
[edit]Is this configuration already retired? — Preceding unsigned comment added by 94.220.12.243 (talk) 08:38, 3 January 2017 (UTC)
- ULA is retiring the the Delta IV Medium versions; the comparable Atlas V versions will be used instead since they cost less. Here's an article about that. -Fnlayson (talk) 15:31, 4 January 2017 (UTC)
Separate Delta IV and Delta Heavy Launches Page?
[edit]Most of the other rockets have separate launches pages, as that information is separate from the vehicles themselves. Should we move that information to a new page? UnknownM1 (talk) 06:18, 19 February 2018 (UTC)
I just noticed there is a weird kind of hybrid page of multiple different rockets, separated by decades, under the "Delta" wing. It is very confusing and sort of unhelpful. It seems that the whole page needs reform or rework. UnknownM1 (talk) 06:20, 19 February 2018 (UTC)
- Note that the Delta Heavy IS still a Delta IV rocket variant. -Finlayson (talk) 13:42, 19 February 2018 (UTC)
- No I am aware. I think it is a List of Thor and Delta Rocket Launches, but the article layout itself is confusing and there shouldn't be the same information on multiple pages. UnknownM1 (talk) 15:50, 19 February 2018 (UTC)
- OK, I just wanted to clarify about keeping them together. Splitting up the launches by rocket model seems clearer than by decade as done with Thor and Delta launches now, imo. -Finlayson (talk) 16:16, 19 February 2018 (UTC)
- No I am aware. I think it is a List of Thor and Delta Rocket Launches, but the article layout itself is confusing and there shouldn't be the same information on multiple pages. UnknownM1 (talk) 15:50, 19 February 2018 (UTC)
- Yes, launches should be grouped by major evolution, i.e. Delta "alpha", Delta "numeric", Delta II + III, Delta IV, Delta IV Heavy. As a rule of thumb, if a rocket version has a dedicated article, it probably deserves a dedicated list of launches. — JFG talk 17:38, 19 February 2018 (UTC)
Number of Launches (in Infobox)
[edit]The Delta IV rocket has launched 39 times, and it even says that later in the article. However, in the infobox it still says it's only launched 37 times. Can that please be updated? SnowballEffect (talk) 23:23, 12 May 2019 (UTC)
- The Infobox has been updated now. You could have just updated them or started on it yourself. -Fnlayson (talk) 00:21, 13 May 2019 (UTC)
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