Что случилось с Аполлоном-9?

After launch and injection of the combined S-IVB stage and the adaptor-LM-CSM payload into a 189.6 x 192.5 km Earth orbit, the S-IVB propellant tanks were vented, changing the orbit to 198 x 204 km. At 2:41 after launch the CSM separated from the S-IVB and and the adaptor panels were jettisoned, exposing the LM mounted on the S-IVB. The CSM turned around and docked with the LM at 3 hours after launch. At 4 hours after launch the S-IVB and CSM-LM were separated and the S-IVB had a 62 second burn to raise its apogee to 3050 km.

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