ApolloHoax.net
Apollo Discussions => The Reality of Apollo => Topic started by: bknight on April 22, 2020, 10:55:43 AM
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A few years ago one of the members helped me "develop" a TLI velocity profile and then a launch to LEO for the Saturn V.
He gave me some wonderful numbers that I have since lost.
What I'm looking for is a table to identify the dry weights of the rockets components and the fuel/oxidizer weights of all the stages.
I searched for Apollo by the numbers but only came up with times distances etc., not the weights. I even have downloaded a few of the Saturn post mission reports but again no weights, just distances and times.
Anyone have a linked source?
ETA: I should have given Robert Braeunig credit for his help.
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What about page 284 of Apollo By The Numbers? Ground Ignition Weights?
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Yes that's it, thanks.
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What about page 284 of Apollo By The Numbers? Ground Ignition Weights?
In case it matters: If it hasn't been amended on the web page, note that oxidizer and fuel figures are reversed for the S-II stage.
It should read:--
S-II stage, dry - 88,500 etc. -->
S-II stage, oxidizer - 793,795 etc. -->
S-II stage, fuel - 154,907 etc. -->
S-II stage, other - 1,426 etc. -->
S-II stage, total - 1,038,628 etc. -->
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What about page 284 of Apollo By The Numbers? Ground Ignition Weights?
In case it matters: If it hasn't been amended on the web page, note that oxidizer and fuel figures are reversed for the S-II stage.
It should read:--
S-II stage, dry - 88,500 etc. -->
S-II stage, oxidizer - 793,795 etc. -->
S-II stage, fuel - 154,907 etc. -->
S-II stage, other - 1,426 etc. -->
S-II stage, total - 1,038,628 etc. -->
Thanks I hadn't gotten to the second stage in my project yet.