Saturn V wieghts

[bknight]

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.

[Obviousman]

What about page 284 of Apollo By The Numbers? Ground Ignition Weights?

[bknight]

Yes that's it, thanks.

[Kiwi]

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. -->

[bknight]

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.