(Translated by https://www.hiragana.jp/)
Talk:Saturn C-3 - Wikipedia Jump to content

Talk:Saturn C-3

Page contents not supported in other languages.
From Wikipedia, the free encyclopedia
[edit]

Hello fellow Wikipedians,

I have just modified one external link on Saturn C-3. Please take a moment to review my edit. If you have any questions, or need the bot to ignore the links, or the page altogether, please visit this simple FaQ for additional information. I made the following changes:

When you have finished reviewing my changes, you may follow the instructions on the template below to fix any issues with the URLs.

This message was posted before February 2018. After February 2018, "External links modified" talk page sections are no longer generated or monitored by InternetArchiveBot. No special action is required regarding these talk page notices, other than regular verification using the archive tool instructions below. Editors have permission to delete these "External links modified" talk page sections if they want to de-clutter talk pages, but see the RfC before doing mass systematic removals. This message is updated dynamically through the template {{source check}} (last update: 5 June 2024).

  • If you have discovered URLs which were erroneously considered dead by the bot, you can report them with this tool.
  • If you found an error with any archives or the URLs themselves, you can fix them with this tool.

Cheers.—InternetArchiveBot (Report bug) 08:19, 11 November 2017 (UTC)[reply]

Stages?

[edit]

The article says "and the two-stage Saturn V's 75,000 kg (165,000 lb) capability...". Two stages? Could the first two stages of the Saturn V put that much in orbit, or is it supposed to be three stages? Bubba73 You talkin' to me? 08:11, 25 June 2019 (UTC)[reply]

Yes, at least. It was used that way to launch Skylab, which weighed 170,000 lb. If memory serves, three-stage orbit capability would have been around 260,000 lb. (People on Wikipedia like to play games with this and base its orbital capability on what the Apollo / S-IVB stack weighed in orbit including its trans-lunar injection fuel, but that's not really correct because that could have been burned to lift an inert payload. That figure was only circulated in early contemporary, hard to find sources dating from the time the Saturn V was in design.) JustinTime55 (talk) 12:49, 25 June 2019 (UTC)[reply]