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COSPAR: 1971-063D. Released from Apollo 15 into 102 x 142 km lunar orbit on 4 August 1971 at 20:13:29 GMT; studied lunar particles and included fields experiments. August 4, in an orbit of 141.Three by 102 kilometers. EDT August 2. About two hours later the LM and CSM rendezvoused and docked, and movie, gear, and 77 kilograms of lunar samples have been transferred from the LM to the CSM. A 40-minute hold had been ordered eight minutes before scheduled launch time because of unsatisfactory weather situations, the primary such delay in the Apollo program. Flight: Apollo 12. Spacecraft: Apollo CSM. After rechecking the techniques in the LM, astronauts Shepard and Mitchell separated the LM from the CSM and descended to the lunar floor. The spacecraft and S-IVB stage entered a parking orbit with a 185.5-kilometer apogee and a 181.5-kilometer perigee. Radiation Meteoroid. Spacecraft engaged in analysis. The lunar module returned to dock successfully with the CSM following the eight-hour separation, and the LM crew returned to the CSM.The LM ascent stage was jettisoned, its batteries have been burned to depletion, and it was positioned in a photo voltaic orbit on May 23. The crew then ready for the return journey to earth and after 61.5 hours in lunar orbit a service propulsion system TEI burn injected the CSM right into a trajectory towards the earth.

Apollo 10 LM – . Call Sign: Intrepid. Payload: Apollo LM 6. Mass: 15,223 kg (33,560 lb). 1971 January 31 – . 1971 July 26 – . EDT July 20. Armstrong reported to mission control at MSC, “Houston, Tranquillity Base here – the Eagle has landed.” (Eagle was the identify given to the Apollo eleven LM; the CSM was named Columbia.) Man’s first step on the moon was taken by Armstrong at 10:Fifty six p.m. Perigee: 303 km (188 mi). Perigee: 185 km (114 mi). Perigee: 184 km (114 mi). Perigee: 170 km (100 mi). Just earlier than reentering the LM, astronaut Shepard dropped a golf ball onto the lunar surface and on the third swing drove the ball 366 meters. Liftoff of the ascent stage of the LM, the primary one to be televised, occurred at 1:11 p.m. After the crew transferred with the samples, gear, and film to the Yankee Clipper, the Intrepid was jettisoned and intentionally crashed onto the lunar floor at 5:17 p.m. The crew and ground personnel were unable to determine why the CSM and LM had did not dock properly, however there was no indication that the methods would not work when used later in the flight.

The seismic sign generated by the affect lasted 3 hours 20 minutes and was so strong that a ground command was necessary to scale back seismometer acquire and keep the recording on the scale. On their return, they adjusted the alignment of the ALSEP central station antenna in an effort to strengthen the signal obtained by the Manned Space Flight Network floor stations again on earth. EST November 19. Through the second EVA, Conrad and Bean retrieved the lunar module Tv digital camera for return to earth for a failure evaluation, obtained photographic panoramas, core and trench samples, a lunar setting sample, and assorted rock, dirt, bedrock, and molten samples. The satellite would measure interplanetary. Inclination: 32.50 deg. Period: 88.19 min. Inclination: 31.12 deg. Period: 88.18 min. Inclination: 32.50 deg. Period: 88.31 min. USAF Sat Cat: 5377 . USAF Sat Cat: 4371 . USAF Sat Cat: 4900 . November 20. The final 24 minutes of the rendezvous sequence was televised. The second EVA had lasted 4 hours 35 minutes, making a total EVA time for the mission of 9 hours 24 minutes.

The stage hit the lunar floor at 4:02 p.m. However, during transposition and docking, CSM one hundred ten Kitty Hawk had issue docking with LM-8 Antares. The CM and SM separated, the parachutes deployed, and other reentry events went as deliberate, and the Kitty Hawk splashed down in mid-Pacific at 4:05 p.m. The lunar surface experiments packages had been deployed, but unintended breaking of the electronics cable rendered the heat movement experiment inoperable. Store away from heat. The first EVA traverse was to the Apennine mountain entrance, after which the ALSEP was deployed and activated, and one probe of a Heat Flow experiment was emplaced. A second probe was not emplaced till EVA-2 because of drilling difficulties. The second extravehicular traverse, which began at 11:33 a.m. A second EVA interval began at 3:Eleven a.m. The primary extravehicular exercise started at 11:Fifty nine a.m. The primary EVA began at 9:Fifty three a.m., after intermittent communications problems in the portable life help system had caused a 49-minute delay. It also carried charged-particle sensors and tools to detect variations in lunar gravity attributable to mascons (mass concentrations).

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