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- 1 Capsule volume discrepancy
- 2 Image on the Left
- 3 g-Forces
- 4 Launch Escape System
- 5 space capsule
- 6 skin
- 7 Last American to orbit the Earth solo
- 8 Mercury 13 section
- 9 Merge
- 10 Interior volume of spacecraft
- 11 Clarification needed
- 12 Cabin volume: source needed
- 13 Mission Profile
- 14 Article insufficiently covers the Mercury spacecraft
- 15 Revision July 2013
- 16 JFK "invited" Glenn to explain delays?
- 17 Cost
- 18 Reentry: pressure vs friction
- 19 which would have been Slayton's flight?
Capsule volume discrepancy
Check out the following differing figures from the article, given for the Mercury capsule's volume:
- Spacecraft section: Only 12.13 cubic meters of volume (...)
- Data table: Volume: 60 ft³ 1.7 m³
I wonder if a typo mighirockt've crept into the Spacecraft sec's number. My guess so far is that the correct number should be, say, 1.213 m³, and that it represents the capsule's internal volume. Any comments? --Wernher 19:54, 12 Oct 2004 (UTC)
-  states that the habitable volume was 1.7m³. There is often a bit of descepancy between various sources on things like volumes, capacities etc. --enceladus 21:23, 12 Oct 2004 (UTC)
It's been 8 years since this discrepancy was pointed out and it's still live... the Mercury did NOT have an internal volume of 12 meters, can we please get it corrected to something CLOSER to reality... or at least smaller then the Apollo CSM's volume? 22.214.171.124 (talk) —Preceding undated comment added 03:22, 14 June 2012 (UTC)
- What are you on about, then? The number has been corrected in the article (1.7 cubic meters), which is about as good as we're likely to get. JustinTime55 (talk) 21:34, 2 October 2012 (UTC)
Image on the Left
What is it? Why is it not labeled?
- It is the Mercury program monument at pad 14. The entry in the article to include the image was missing the word "thumb". I believe that I have fixed it. Vaoverland 12:37, 13 November 2006 (UTC)
During reentry, the astronaut would experience about 4 g-forces. The separate mission articles say otherwise: Mercury-Redstone 3: 11.6 g, Mercury-Redstone 4: 11.1 g, Mercury-Atlas 6: 7.7 g, Mercury-Atlas 7: 7.8 g, Mercury-Atlas 7: 8.1 g, Mercury-Atlas 9: 7.6 g. So this might need to be corrected. --Proofreader 18:16, 10 January 2007 (UTC)
Not necessarily; the booster numbers are obviously giving the launch accelleration. Re-entry g-force is completely different, caused by the friction of the air, and is totally unrelated to the acceleration at launch, and would mainly be driven by re-entry speed. I would expect the orbital flights (M-A) to be perhaps a bit different (bigger?) than the suborbitals (M-R).JustinTime55 (talk) 22:29, 26 February 2010 (UTC)
- Opps--I mis-spoke. The articles explicitly quote re-entry g's and are fuzzy or silent about the launch g's, so Proofreader is correct. The sub-orbitals probably pulled much higher re-entry g's because of the steeper ballistic trajectory. JustinTime55 (talk) 22:47, 26 February 2010 (UTC)
Launch Escape System
The article says the LES generated 52,000 lbs of thrust. With a launch weight of 4265 lbs, that works out to a little over 11 Gs. Is that really possible? Can people survive 11 Gs? -- RoySmith (talk) 01:29, 5 May 2008 (UTC)
reading John Glenn's memoir just recently, 16 gs was the max survivable "upper limit" that they found they could subject astronauts to if they had to and still be ok (due to heart/lung issues). Yes the LES would have kicked it higher very briefly, I imagine if it had come down to that kind of emergency situation they figure better to have the astronanut alive if hurt then nothing at all. —Preceding unsigned comment added by 126.96.36.199 (talk) 19:23, 23 January 2009 (UTC)
From what i've seen looking @ a few references, each capsule was built with some minor differences as they went along. Mainly I've seen the corrugated parts on the upper as opposed to the lower part of the capsules. For exmaple "The Recovery Section had corrugated Rene 41 shingles rather than the flat plate-type beryllium shingles used on manned flights." also "MR-2 and MR-3 were also unique in having a different main hatch. These two missions had a thick hatch with a relatively smooth surface, not corrugated like the shingles covering the capsule." so not positive but I would guess for strength mainly, as the LES was conected to that part up top. —Preceding unsigned comment added by 188.8.131.52 (talk) 19:31, 23 January 2009 (UTC)
- Actually, those corrugations you see on the Mercury spacecraft are for keeping it cool rather than for strength. What you're looking at are the outer "shingles" on the spacecraft. The spacecraft's structural skin, which provides the strength, lies underneath the shingles. The shingles are corrugated to increase their surface area. That would give the spacecraft more surface area from which to radiate heat away into space while absorbing the same amount of sunlight.
- I think they might also provide more surface area for air to flow over during atmospheric reentry, which would help remove heat during that stage. That would explain why the shingle corrugations run across the direction of airflow, rather than parallel to it as you might expect. That does increase drag, but only by a very small amount compared to the blunt heatshield, and the relatively slow turbulent airflow over the corrugations would efficiently carry away the heat that was conducted from the heatshield to the rest of the spacecraft.
- During launch, the corrugations wouldn't increase the drag that much. The sharp aerospike at the tip of the escape rocket did a lot to reduce drag during the supersonic portion of the launch, when drag was at its worst, because it caused the supersonic shock wave to build up ahead of the rocket's main body.
Last American to orbit the Earth solo
The article describes Gordon Cooper as the "Last American to orbit the Earth solo", but isn't that actually David Scott, the Command Module pilot of Apollo 9? He orbited the Earth solo while the Lunar Module was being test flown. 184.108.40.206 (talk) 03:09, 27 July 2009 (UTC)
- Cooper was the last American to orbit the Earth solo. No one else was in orbit at the time. To be more definitive, though, he was unequivocally the last American to be launched into orbit alone. —Preceding unsigned comment added by SEWalk (talk • contribs) 02:58, 23 October 2009 (UTC)
- Bruce McCandless could also be considered an astronaut flying in solo orbit. I have modified the table remark. ShelbyBell (talk) 23:30, 24 June 2012 (UTC)
Mercury 13 section
- There have been no objections, so I removed that section. It is mentioned in the See also section. Bubba73 (You talkin' to me?), 15:24, 15 July 2010 (UTC)
The removal of the lists of unmanned and manned Mercury launches diminishes the utility of this article, to no discernible purpose. Relevant information should be grouped together for easy reference and comparison; having to go to several different articles for the relevant information significantly impairs the encyclopedic usefulness of the article. RandomCritic (talk) 03:42, 28 October 2011 (UTC)
- Since there was no objection, I completed the merge. RandomCritic (talk) 19:06, 15 November 2011 (UTC)
Interior volume of spacecraft
I had changed cubic meters to decimeters/liters since cubic meters seemed like a large metric to describe the volume and used both cubic decimeters and liters because cubic decimeters are the recognized but uncommon SI unit. I also added cubic feet in parentheses for three reasons:
1. The spacecraft was built by McDonnel in the 1950s in the US, and most likely designed to specifications described in US customary units.
2. As a convenience and courtesy to the smaller yet significant portion of the English language wikipedia readers who lack an intuitive scope of area defined by SI units.
3. A secondary metric of 60 cubic feet is also helpful to those readers familiar with both SI and US customary units.
The change was reverted, and while I concede to the reversion of the SI volume back to "cubic meters" on the proposed basis that liters are not as intuitive as cubic meters when describing volume, I object to the removal of the secondary metric given in "cubic feet". I intend to edit the secondary metric using "cubic feet" following "cubic meters" into the article in parentheses following the primary description in cubic feet. If it is removed afterwards I will accept the change and refrain from editing this detail in the future.
After reading the cited link, I discovered that the original interior dimensions were incorrect in the first place. According to centennialofflight.net a website designed to provide public information on the history powered human flight run by the US government who also commissioned, owned and operated every Mercury spacecraft that was produced:
"The spacecraft that was designed was cone-shaped with a cylinder on top. It was 6.8 feet (2 meters) long, 6.2 feet (2 meters) in diameter, and had a 19.2-foot, (5.8-meter) escape tower with a solid-rocket motor fastened to the cylinder. In a launch emergency, the rocket would fire and lift the capsule from an explosion and parachute it into the ocean. With a volume of only 428.5 cubic feet (12 cubic meters), there was barely enough room for its pilot, who sat in a custom-designed couch facing a panel with 120 controls, 55 electrical switches, 30 fuses, and 35 mechanical levers. The cabin's atmospheric pressure was one-third of that on Earth and contained pure oxygen." 
So while I previously stated I would no longer edit this detail, I must revise that to I will not reinsert the non SI metric if it is reverted but will ensure the proper SI metric of "12 cubic meters" is maintained if reverted back to the incorrect "1.7 cubic meters" metric.
(and just to be clear, my use of the term "metric" in these comments is not a reference to the "Metric System" but as a term describing any generic measurement irregardless* of the scale used)
- just kidding, I know the word is "regardless" sorry for those it made cringe.
- Thank you for obtaining the accurate volume number. And thanks so much for your "convenience and courtesy" extended to the "smaller yet significant portion". There is a strong national tie to Project Mercury, since it was undertaken by the US, which in 1958 did not (and to this day, still in most of the aerospace industry, does not primarily) use metric units; therefore the English units should go first. That's the most authoritative way to obtain the correct value for the historical US space programs, as that was what was originally used in the design, and the metrics were/are a conversion extended as a courtesy. (NASA didn't switch officially to metric units until the 1970's.) We also have the Template:convert to maintain accurate unit conversions. JustinTime55 (talk) 16:28, 6 June 2012 (UTC)
- Please see: Talk:Project Mercury#Capsule volume discrepancy, is this helpful? Soerfm (talk) 14:25, 4 April 2012 (UTC)
I have a problem understanding just what this sentence is trying to say:
- "Twelve companies bid to build the Mercury spacecraft, an unusually high number for a $20 million contract, given the project's great prestige."
Exactly why would one expect fewer than 12 contractors to bid? The $20 million is in 1958 U.S. dollars, which doesn't give modern readers a good handle on it (would be equivalent to much more today.) And what is the assumed relationship of price to attraction? (One would assume it's positive.) And then, "given the project's great prestige" is thrown in at the end, which should attract more bidders. The use of "given" is confusing, and probably not what you intended? The phrase "given [the fact that...]" is usually used to reinforce an expectation when used in such a sentence. Is this the essence of what you were trying to say?
- "It was surprising that as many as 12 contractors bid, since [here's where "given" would be more appropriate], it was only worth $20 million; yet it had a great deal of prestige."
Cabin volume: source needed
The US Centennial of Flight Commission has a mistake on its Mercury page; the volume of the capsule could not possibly be 428.5 cubic feet, when the Apollo Command Module had only 218 cubic feet. (This is why we need verification!) I believe the 60. figure, because I tabulated a comparison with the others (Vostok for reference, is 63 cubic feet) but unfortunately I can't remember where I got that. Can someone help, please? JustinTime55 (talk) 21:27, 13 July 2012 (UTC)
In the mission profile page it talks about how the orbital version needed a bigger rocket as compared to the sub-orbital version so that it can achieve a "higher altitude". This is misleading, the biggest reason why an orbital mission needs a more powerful rocket is the substantially higher speed needed to achieve orbit. 220.127.116.11 (talk) 04:44, 19 July 2012 (UTC)
Article insufficiently covers the Mercury spacecraft
This was the article a year ago, this is it now. A lot of information was removed for reasons not entirely clear to me, if it was removed because someone believed it was beyond the scope of the article than a page should have been created specifically for the Mercury spacecraft. Can we do anything to rectify this?--Craigboy (talk) 02:29, 29 September 2012 (UTC)
Revision July 2013
I have made a revision mostly based on
- Alexander, C. C.; Grimwood, J. M.; Swenson, L. S. (1966). This New Ocean: a History of Project Mercury. USA: NASA. ISBN 1934941875.
- Catchpole, John (2001). Project Mercury - NASA's First Manned Space Programme. Chichester, UK: Springer Praxis. ISBN 1-85233-406-1.
I have deleted some information:
- claim in lead about planet Mercury (original research and not verified in body)
- claim about spacecraft being worn not ridden (no citation)
- claim about minor participants (no citation)
- claim that MJ-1 was proposed as a heat shield test (no citation)
- claim that MJ-2 was deemed unnecessary (no citation, contradicts budget constraint claim)
I reduced the information about T.J. O'Malley pushing the button to a footnote. I found a citation for the volume of the spacecraft, on the other hand, but it was 100 cubic feet and not 60 cubic feet. As requested, I have expanded the spacecraft section. I have also maximized the use of pictures. Finaly, I have deleted dead links and links overlapping Bibliography from External links section.
JFK "invited" Glenn to explain delays?
This dubious footnote was just added:
- "...a frustrated politician compared the spacecraft-Atlas combination to "a Rube Goldberg device on top of a plumber's nightmare" and John Glenn was invited to the White House to explain the delays."
This New Ocean verifies the senator's remark, but makes it clear that JFK, while disappointed like everyone else, believed NASA knew best what was required to make the flight with reasonable safety, and describes Glenn's February visit (incidental to his visiting family in Virginia) as "a brief visit with President Kennedy, who asked him many semitechnical questions about plans and systems for the orbital flight" (citing several newspaper reports), but says nothing at all about Kennedy demanding Glenn "explain delays". This would seem totally out of character for JFK; I removed it. I have no idea who this Brit John Catchpole is, but I would suggest being cautious about regarding his Project Mercury - NASA's First Manned Space Programme as a reliable source about certain things. JustinTime55 (talk) 17:32, 18 September 2013 (UTC)
- I think you are right, putting information together like that tends to be OR. Maybe it should be stressed that the two are not related: On the one hand people made jokes about the project on the other John Glenn And JFK had an informal meeting to fill out the wait before the launch of MA-6. Soerfm (talk) 18:24, 18 September 2013 (UTC)
"It is estimated to have cost $1.71 billion and have involved the work of 2 million people." - this should be clarified to specify either the cost in 1950s/60s dollars, or the cost in ~2013 dollars. Apparently this is the cost accounting for inflation? — Preceding unsigned comment added by 18.104.22.168 (talk) 13:49, 11 October 2013 (UTC)
- Look further: in the infobox and down in the article body, it says that's today's cost. JustinTime55 (talk) 16:46, 11 October 2013 (UTC)
Reentry: pressure vs friction
Both pressure and friction seem to create heat during reentry...
The Ames researcher determined that the amount of heat absorbed by an object descending into the atmosphere depended on the ratio between pressure drag and viscous or frictional drag. The designer of a reentry body, by shaping the body bluntly, could alter pressure drag and thus throw off much of the heat into the surrounding air.— This New Ocean, p 61.
- You are probably referring to my revert of the anon's change of the page text on this issue. As the issue is more complex than either friction or a pressure wave and the change was not ref'd, I reverted it assuming I'd come back to it later (which I didn't). That being said, the sentence probably needs to be changed to reflect the more complex description of what is actually going on. The returning capsule causes the atmosphere to be compressed and heated while the bow shock causes frictional drag - both of which contribute to the capsules heating. Ckruschke (talk) 13:53, 8 November 2013 (UTC)Ckruschke
which would have been Slayton's flight?
Does anyone know which of the cancelled flights would have been Deke Slayton's before he was grounded? Slayton's Wiki article says he was supposed to fly on the second orbital flight - named Delta 7 - but his place was taken by Scott Carpenter, on Aurora 7. My main question is, which of the cancelled flights would have been flown by Slayton? And did Carpenter simply replace Slayton, or was Carpenter's flight moved up and Slayton's cancelled outright? Elsquared (talk) 00:02, 30 November 2013 (UTC)
- . United States government http://www.centennialofflight.net/essay/SPACEFLIGHT/Mercury/SP17.htm. Missing or empty