The two astronauts transferred from the LM to the CSM with samples, gear, and movie. Stationkeeping was initiated about seven and one-half hours after liftoff, and hard docking was achieved about 30 minutes later following two unsuccessful docking attempts. Two midcourse corrections were made on the return flight to attain the specified entry interface conditions. Increased manned house flight time record by 50%. Rebellion by crew against NASA Ground Control overtasking led to none of the crew ever flying again. LM angle management was lost at jettison; due to this fact a deorbit maneuver was not potential and the LM remained in lunar orbit, with an estimated orbital lifetime of about one year. During the rendezvous, the CSM response management system forward firing engine oxidizer valve leaked. S-IVB auxiliary propulsion system burns sent the S-IVB/IU levels toward the moon, the place they impacted the lunar floor at 4:59 p.m. Tests and analyses showed the redundant system to be still protected and usable if required. At 1:08 p.m., onboard color Tv confirmed the docking of the CSM with the LM. Docking maneuver was wonderful. Station-conserving with the Saturn Workshop began approximately 8 hours after liftoff, with docking being carried out about 30 minutes later. The rendezvous sequence was carried out based on the anticipated timeline.
The second plane-change maneuver and some orbital science pictures have been deleted so that transearth injection could be performed about 24 hours earlier than originally deliberate. Translunar injection was at about 12:30 p.m., with separation of the CSM from the LM/S-IVB/IU at 12:Fifty six p.m. A transearth injection maneuver at 5:23 p.m. Apollo 16 entered a lunar orbit of 314 by 107.7 kilometers at 3:22 p.m. Loss of all subsatellite monitoring and telemetry data on the 425th revolution (May 29) indicated that the subsatellite had hit the lunar surface. Hit the lunar surface at 11:04 p.m.m. Intentionally crashed on the moon’s surface at 7:Forty six p.m.m. The lunar floor experiments packages have been deployed, but unintentional breaking of the electronics cable rendered the heat circulation experiment inoperable. Activities through the transearth coast phase of the mission included pictures for a contamination examine for the Skylab program. Then began the second planned traverse of the mission. The crew then drove in a northwesterly course, making stops close to Stubby and Wreck Craters. The crew then returned by way of the experiment station to the lunar module. Accomplished 858 Earth orbits and 1,081 hours of photo voltaic and Earth experiments; three EVAs totalled 13 hours, forty three minutes.The area car, consisting of a modified Apollo command and service module payload on a Saturn IB launch car, was inserted into a 231.3 by 154.7 km orbit.