Gemini 10 (officially Gemini X) was a 1966 crewed spaceflight in NASA's Gemini program. It was the 8th crewed Gemini flight, the 16th crewed American flight, and the 24th spaceflight of all time (includes X-15 flights over 100 kilometers (54 nautical miles)).
Gemini 10 is boosted into a higher orbit by its Agena Target Vehicle
|Mission duration||2 days, 22 hours, 46 minutes, 39 seconds|
|Launch mass||8,295 pounds (3,762.6 kg)|
|Landing mass||4,254 pounds (1,930 kg)|
|Members||John W. Young|
|EVA duration||1 hour, 28 minutes|
|Start of mission|
|Launch date||July 18, 1966, 22:20:26UTC|
|Rocket||Titan II GLV, s/n #62-12565|
|Launch site||Cape Kennedy LC-19|
|End of mission|
|Recovered by||USS Guadalcanal|
|Landing date||July 21, 1966, 21:07:05UTC|
|Regime||Low Earth orbit|
|Perigee altitude||161 nautical miles (299 km)|
|Apogee altitude||408 nautical miles (756 km)|
|Epoch||July 19, 1966|
|Docking with GATV-5005|
|Docking date||July 19, 1966, 04:15:00 UTC|
|Undocking date||July 20, 1966, 19:00:00 UTC|
|Time docked||1 day, 14 hours, 45 minutes|
(L-R) Young, Collins
|Command Pilot||John W. Young|
|Command Pilot||Alan L. Bean|
|Pilot||Clifton C. Williams, Jr.|
Jim Lovell and Buzz Aldrin had originally been named the backup crew, but after Charles Bassett and Elliot See died in a T-38 crash, they were moved to the backup crew for Gemini 9 and Alan Bean and Clifton Williams were moved to the Gemini 10 flight.:123
- Mass: 8,295 pounds (3,762.6 kg)
- Perigee: 86.3 nautical miles (159.9 km)
- Apogee: 145.2 nautical miles (268.9 km)
- Inclination: 28.87°
- Period: 88.79 min
- Docked: July 19, 1966 - 04:15:00 UTC
- Undocked: July 20, 1966 - 19:00:00 UTC
- Collins - EVA 1 (stand up)
- Start: July 19, 1966, 21:44:00 UTC
- End: July 19, 1966, 22:33:00 UTC
- Duration: 0 hours, 49 minutes
- Collins - EVA 2
- Start: July 20, 1966, 23:01:00 UTC
- End: July 20, 1966, 23:40:00 UTC
- Duration: 0 hours, 39 minutes
Gemini 10 established that radiation at high altitude was not a problem. After docking with their Agena booster in low orbit, Young and Collins used it to climb temporarily to 412.4 nautical miles (763.8 km). After leaving the first Agena, they then rendezvoused with the derelict Agena left over from the aborted Gemini 8 flight—thus executing the program's first double rendezvous. With no electricity on board the second Agena, the rendezvous was accomplished with eyes only—no radar.
After the rendezvous, Collins spacewalked over to the dormant Agena at the end of a 50-foot (15 m) tether, making him the first person to meet another spacecraft in orbit. Collins then retrieved a cosmic dust-collecting panel from the side of the Agena. As he was concentrating on keeping his tether clear of the Gemini and Agena, Collins' Hasselblad camera worked itself free and drifted away, so he was unable to take photographs during the spacewalk.
Gemini 10 was designed to achieve the objectives planned for the last two missions—rendezvous, docking and EVA. It also hoped to dock with the Agena Target Vehicle from the Gemini 8 mission. This Agena's battery power had failed months earlier, and an approach and docking would demonstrate the ability to rendezvous with a passive object. It would be also the first mission to fire the Agena's own rocket, allowing them to reach higher orbits.
The Agena launched perfectly for the second time, after problems had occurred with the targets for Gemini 6 and 9. Gemini 10 followed 100 minutes later and entered a 86.3-by-145.2-nautical-mile (159.9 by 268.9 km) orbit. They were 970 nautical miles (1,800 km) behind the Agena. Two anomalous events occurred during the launch. At liftoff, a propellant fill umbilical became snared with its release lanyard. It ripped out of the LC-19 service tower and remained attached to the second stage during ascent. Tracking camera footage also showed that the first stage oxidizer tank dome ruptured after staging and released a cloud of nitrogen tetroxide. The telemetry package on the first stage had been disabled at staging, so visual evidence was the only data available. Film review of the Titan II ICBM launches found at least seven other instances of post-staging tank ruptures, most likely caused by flying debris, second stage engine exhaust, or structural bending. NASA finally decided that this phenomenon did not pose any safety risk to the astronauts and took no corrective action.
|Gemini 10||Agena Info|
|Mass||7,000 pounds (3,175 kg)|
|Launch date||July 18, 1966|
|Launch time||20:39:46 UTC|
|1st perigee||159.1 nautical miles (294.7 km)|
|1st apogee||163.5 nautical miles (302.8 km)|
|Reentered||December 29, 1966|
Collins was unable to use the sextant for navigation as it did not seem to work as expected. At first he mistook airglow as the real horizon when trying to make some fixes on stars. When the image didn't seem right he tried another instrument, but this was not practical to use as it had a very small field of view.
They had a backup in the form of the computers on the ground. They made their first burn to put them into a 143-by-147-nautical-mile (265 by 272 km) orbit. However Young didn't realize that during the next burn, he had the spacecraft turned slightly, which meant that they introduced an out-of-plane error. This meant two extra burns were necessary, and by the time they had docked with the Agena, 60% of their fuel had been consumed. It was decided to keep the Gemini docked to the Agena as long as possible, as this would mean that they could use the fuel on board the Agena for attitude control.
The first burn of the Agena engine lasted 80 seconds and put them in a 159-by-412-nautical-mile (294 by 763 km) orbit. This was the highest a person had ever been, although the record was soon surpassed by Gemini 11, which went to over 540 nautical miles (1,000 km). This burn was quite a ride for the crew. Because the Gemini and Agena docked nose-to-nose, the forces experienced were "eyeballs out" as opposed to "eyeballs in" for a launch from Earth. The crew took a couple of pictures when they reached apogee but were more interested in what was going on in the spacecraft — checking the systems and watching the radiation dosage meter.
After this they had their sleep period which lasted for eight hours and then they were ready for another busy day. The crew's first order of business was to make a second burn with the Agena engine to put them into the same orbit as the Gemini 8 Agena. This was at 20:58 UTC on July 19 and lasted 78 seconds and took 340 feet per second (105 m/s) off their speed, putting them into a 159-by-206-nautical-mile (294 by 382 km) orbit. They made one more burn of the Agena to circularize their orbit to 203.9 nautical miles (377.6 km).
The first of two EVAs on Gemini 10 was a standup EVA, where Collins would stand in the open hatch and take photographs of stars as part of experiment S-13. They used a 70 mm general purpose camera to image the southern Milky Way in ultraviolet. After orbital sunrise Collins photographed a color plate on the side of the spacecraft (MSC-8) to see whether film reproduced colors accurately in space. He reentered the spacecraft six minutes early when both astronauts found that their eyes were irritated, which was caused by a minor leak of lithium hydroxide in the astronauts' oxygen supply. After repressurizing the cabin, they ran the oxygen at high rates and flushed the environment system.
After the exercise of the EVA Young and Collins slept in their second 'night' in space. The next 'morning' they started preparing for the second rendezvous and another EVA.
After undocking from their Agena, the crew thought they sighted the Gemini 8 Agena. It however turned out to be their own Agena 3.0 nautical miles (5.5 km) away, while their target was 95 nautical miles (176 km) away. It wasn't until just over 16 nautical miles (30 km) away that they saw it as a faint star. After a few more correction burns, they were station-keeping 10 feet (3.0 m) away from the Gemini 8 Agena. They found the Agena to be very stable and in good condition.
At 48 hours and 41 minutes into the mission, the second EVA began. Collins' first task was to retrieve a Micrometeorite Collector (S-12) from the side of the spacecraft. This he accomplished with some difficulty (similar to that encountered by Eugene Cernan on Gemini 9A). The collector floated out of the cabin at some time during the EVA, and was lost.
Collins next traveled over to the Agena and tried to grab onto the docking cone but found this impossible as it was smooth and had no grip. He used a nitrogen-propelled Hand-Held Maneuvering Unit (HHMU) to move himself towards the Gemini and then back to the Agena. This time he was able to grab hold of some wire bundles and retrieved the Micrometeorite Collector (S-10) from the Agena. He decided against replacing it as a piece of shroud had come loose on the Agena which could have snared the umbilical, and returning to the Gemini was deemed the safest course of action.
The last tasks remaining on this EVA were to test out the HHMU, test orbital mechanics using a tether between the Gemini and Agena, and for Young in the spacecraft to translate over to a passive Collins. However, due to low propellant quantity remaining, combined with intermittent telemetry to monitor it, these fuel costly manoeuvres were abandoned and the EVA was finished after only 39 minutes. During this time, it took the crew eight minutes to close the hatch as they had some difficulty with the 50-foot (15 m) umbilical. It was jettisoned along with the chestpack used by Collins an hour later when they opened the hatch for the third and final time.
There were ten other experiments that the crew performed during the mission. Three were interested in radiation: MSC-3 was the Tri-Axis Magnetometer which measured levels in the South Atlantic Anomaly. There was also MSC-6, a beta spectrometer, which measured potential radiation doses for Apollo missions, and MSC-7, a bremsstrahlung spectrometer which detected radiation flux as a function of energy when the spacecraft passed through the South Atlantic Anomaly.
S-26 investigated the ion and electron wake of the spacecraft. This provided limited results due to the lack of fuel for attitude control, but found that electron and ion temperatures were higher than expected and it registered shock effects during docking and undocking.
The S-5 and S-6 experiments were performed, which were previously carried on Gemini 9A; these were Synoptic Terrain and Synoptic Weather photography respectively. There was also S-1 which was intended to image the Zodiacal light. All of these experiments were of little use as the film used was only half as sensitive as Gemini 9A and the dirty windows lowered the transmission of light by a factor of six.
The crew also tried to perform D-5, a navigation experiment. They were only able to track five stars, with six needed for accurate measurements. The last experiment, D-10, was to investigate an ion-sensing attitude control system. This experiment measured the attitude of the spacecraft from the flow of ions and electrons around the spacecraft in orbit. The results from this experiment showed the system to be accurate and responsive.
The last day of the mission was short and retrofire came at 70 hours and 10 minutes into the mission. They landed only 3.0 nautical miles (5.6 km) away from the intended landing site and were recovered by USS Guadalcanal.
The Gemini 10 mission was supported by the following U.S. Department of Defense resources: 9,067 personnel, 78 aircraft and 13 ships.
The patch is simple in design but highly symbolic. The main feature is a large X with a Gemini and Agena orbiting around it. The two stars have a variety of meanings: the two rendezvous attempts, Castor and Pollux in Gemini or the two crew members. This is one of the few crew patches without the crew's name. It is able to be displayed "upside down" but is correctly shown with the spacecraft to the right. It was designed by Young's first wife, Barbara.
- McDowell, Jonathan. "SATCAT". Jonathan's Space Pages. Retrieved March 23, 2014.
- Hacker, Barton C.; Grimwood, James M. (September 1974). "Chapter 11 Pillars of Confidence". On the Shoulders of Titans: A History of Project Gemini. NASA History Series. SP-4203. NASA. p. 239. With Gemini IV, NASA changed to Roman numerals for Gemini mission designations.
- "Astronaut Fact Book" (PDF). NASA. April 2013. Retrieved April 18, 2018.
- Reichl, Eugen (2016). Project Gemini. America in Space. Atglen, Pennsylvania: Schiffer Publishing. ISBN 9780764350702.
- "Gemini 10". NASA Space Science Data Coordinated Archive. Retrieved January 6, 2018.
- Collins, Michael (1974). "8". Carrying the Fire: An Astronaut's Journeys (ebook). Cooper Square Press. ISBN 9781461660880.
- "Gemini X Composite Air-to-Ground and Onboard Voice Tape Transcription, 338 pages" (PDF). Retrieved 2 January 2019.
- "Gemini X PAO Mission Commentary Transcript, 524 pages" (PDF). Retrieved 2 January 2019.
- "Gemini X PAO Mission Commentary Transcript, 524 pages" (PDF). Retrieved 2 January 2019.
|Wikimedia Commons has media related to Gemini 10.|
- NASA Gemini 10 press kit - July 15, 1966
- Gemini 10 Mission Report (PDF) August 1966
- Spaceflight Mission Patches: http://www.genedorr.com/patches/Intro.html
- U.S. Space Objects Registry https://web.archive.org/web/20090521121750/http://usspaceobjectsregistry.state.gov/search/index.cfm