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Mission control personnel in Houston. All targets have been achieved besides one experiment – evaluation of the minimal reaction energy tool – which was not performed as a result of umbilical EVA was terminated prematurely. One half minutes. The deliberate entry velocity was 10.61 kilometers per second, while the actual velocity achieved was 10.70.Recovery time of two hours 28 minutes was longer than anticipated, with the cause listed as sea conditions – 2.4-meter swells. Rendezvous was achieved at 3 hours 46 minutes ground elapsed time, docking 28 minutes later. The S-II stage ignition occurred at 2 minutes 32 seconds and the burn lasted 6 minutes 7 seconds, adopted by the S-IVB stage ignition and burn of two minutes 25 seconds. The third stage (S-IVB) firing was additionally longer than planned and at termination of thrust the orbit was 177.7 x 362.9 kilometers relatively than the 160.9-kilometer close to-circular orbit deliberate. Flight of LM-1 also went as planned as much as the first descent propulsion engine firing. A number of spacecraft systems suffered issues in the course of the flight.

LV Family: Titan. Launch Car: Titan II GLV. LV Family: Atlas. Launch Vehicle: Atlas SLV-three Agena D. Gemini 10 Agena Target – . LV Family: Saturn I. Launch Vehicle: Saturn IB. Apollo 8 (AS-503) was launched from KSC Launch Complicated 39, Pad A, at 7:51 a.m. Collins area walks from Gemini to Agena to retrieve micrometeorite package left in space all these months. Because the SPS was used to attain the specified excessive apogee, there was insufficient propellant left to achieve the high-velocity improve desired for the entry. EST January 23, LM levels have been left in orbit to reenter the ambiance later and disintegrate. Spacecraft No. 10 was inserted right into a 145- by 86-nautical-mile elliptical orbit. Five maneuvers completed the spacecraft/GATV rendezvous at 1 hour 25 minutes floor elapsed time, and the 2 autos docked nine minutes later. In the course of the six hours following insertion, the spacecraft completed nine maneuvers to rendezvous with the GATV. Nine spacecraft maneuvers effected rendezvous with the GATV. After two revolutions in a parking orbit, throughout which the systems were checked, operational exams performed, and a number of other angle maneuvers made, preparations were completed for the S-IVB engine restart.

Secondary targets included rendezvous and docking during the fourth revolution, performing docked maneuvers using the GATV primary propulsion system, executing 10 experiments, conducting docking practice, performing a rerendezvous, evaluating the auxiliary tape reminiscence unit, demonstrating controlled reentry, and parking the GATV in a 220-nautical mile circular orbit. In consequence, several experiments weren’t accomplished, and another secondary goal – docking practice – was not attempted. Nonetheless, the ATDA shroud had not utterly separated, thus making docking impossible. Tether connected by Gordon to Agena in spacewalk and after lots of effort tethered spacecraft put into slow rotation, creating first artificial microgravity.The primary goal of the Gemini XI mission was to rendezvous with the Gemini Agena goal vehicle (GATV) throughout the primary revolution and dock. After mission completion at 2:Forty five a.m. Mason at 1:37 a.m. Liftoff got here at 11:03 a.m. Final separation maneuver was performed at 22 hours fifty nine minutes after liftoff. The remaining second-stage engines shut down at 9 minutes 36 seconds – fifty eight seconds later than planned.The S-IVB engine throughout its first burn, which was regular, operated 29 seconds longer than programmed. The tether evaluation started at forty seven hours 23 minutes after liftoff, with the crew undocking from the GATV.

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