NASA What did Apollo CM use helium for?

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Helium tanks in the Apollo Command Module were utilized to feed propellant for the attitude control system and the main engine. These tanks were part of the Command Module's reaction control subsystem. Attitude control thrusters were essential for re-entry, especially after the Service Module was jettisoned. The discussion highlights the importance of helium in managing spacecraft orientation during critical phases of the mission. Understanding these components is crucial for comprehending the Apollo program's engineering.
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Why were there tanks of helium on the CM?
Hello All

Diagrams of the Apollo Command Module show tanks of helium, What was this used for?

best regards ... Stef
 
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I think it was used to feed propellent for attitude control and perhaps the big engine. Were these in the Service module or the command module?
 
Of course you would still need attitude control thrusters for re-entry (after ejecting the Service module). Duh I didn't even think it through.
 
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
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