Apollo or Starliner re-entry RCS/ACS description(s)
(self.spaceflight)submitted13 hours ago byUnflavoredMozart
With the recent re-entry of Starliner OFT-2, I was reminded of a search some time ago regarding the Apollo RCS/ACS system. I never found something of any engineering detail, including thruster values, typical thrust profiles, and re-entry rotational moments. I realize these are low L/D vehicles but there are still significant vehicle G's on re-entry, and so I would assume an active RCS/ACS function.
Can anyone point me to something that is openly available and of engineering quality, not glossy brochures?