Apollo 10

By 1967, NASA had planned the steps that needed to be taken prior to an attempt to land on the Moon. It approved a list of mission types, designated by letters, that needed to be flown prior to a landing attempt, which would be the "G" mission. The early uncrewed flights were considered "A" or "B" missions, while Apollo 7, the crewed-flight test of the Command and Service Module (CSM), was the "C" mission. The first crewed orbital test of the Lunar Module (LM) was accomplished on Apollo 9, the "D" mission. Apollo 8, flown to the Moon's orbit without an LM, was considered a "C-prime" mission, but its success gave NASA the confidence to skip the "E" mission, which was planned to be testing of the full Apollo spacecraft in medium or high Earth orbit. Apollo 10, the dress rehearsal for the lunar landing, was to be the "F" mission.[5][6]

NASA considered skipping the "F" mission as well and attempting the first lunar landing on Apollo 10. Some with the agency advocated this, feeling it senseless to bring astronauts so close to the lunar surface, only to turn away. Although the lunar module intended for Apollo 10 was too heavy to perform the lunar mission, the one intended for Apollo 11 could be substituted by delaying Apollo 10 a month from its May 1969 planned launch.[7] NASA official George Mueller favored a landing attempt on Apollo 10; he was known for his aggressive approach to moving the Apollo program forward.[8] However, Director of Flight Operations Christopher C. Kraft and others opposed this, feeling that new procedures would have to be developed for a rendezvous in lunar orbit, and that NASA had incomplete information regarding the Moon's mass concentrations, which might throw off the spacecrafts' trajectory. Lieutenant General Sam Phillips, the Apollo Program Manager, listened to the arguments on both sides and decided that having a dress rehearsal was crucial.[7]

On November 13, 1968, NASA announced who the crew of Apollo 10 would be.[5] Thomas P. Stafford, the commander, was 38 years old at the time of the mission. A 1952 graduate of the Naval Academy, he was commissioned in the Air Force. Selected as one of the second group of astronauts in 1962, he flew as pilot of Gemini 6A (1965) and command pilot of Gemini 9A (1966).[9] John Young, the command module pilot, was 38 years old and a commander in the Navy at the time of Apollo 10. A 1952 graduate of Georgia Tech who entered the Navy after graduation and became a test pilot in 1959, he was selected as a Group 2 astronaut alongside Stafford. He flew in Gemini 3 with Gus Grissom in 1965, becoming the first American not of the Mercury Seven to fly in space. Young thereafter commanded Gemini 10 (1966), flying with Michael Collins.[10][11] Eugene Cernan, the lunar module pilot, was a 35-year-old commander in the Navy at the time of Apollo 10. A 1952 graduate of Purdue University, he entered the Navy after graduation. Selected as one of the third group of astronauts in 1963, Cernan flew with Stafford on Gemini 9A before his assignment to Apollo 10.[12] With five prior flights among them, Apollo 10 had the most experienced American crew to reach space prior to the Space Shuttle era,[13] and the first American space mission to have a crew consisting entirely of spaceflight veterans.[14]

As Apollo flights were planned in 1966, Stafford was announced as backup CMP for the second crewed Apollo flight, planned as an extended test of the command module, and dubbed Apollo 2, with Frank Borman as backup commander and Collins as backup LMP.[15] After the prime crew of Apollo 2, led by Wally Schirra, went to NASA management with a list of demands concerning their mission, Apollo 2 was cancelled in November 1966, and Stafford was assigned as backup commander for the second Apollo mission under a new schedule, planned to involve the first crewed flight of the lunar module, to be commanded by James McDivitt,with Young as backup CMP and Cernan as backup LMP.[16][17] The Apollo 1 fire in January 1967 led to a rescheduling of Apollo flights, and Stafford's crew was assigned as backups for the first crewed fight.[18] which became Apollo 7, flown by Schirra's crew.[19]

The backup crew for Apollo 10 was L. Gordon Cooper as commander, Donn F. Eisele as command module pilot and Edgar Mitchell as lunar module pilot. By the normal rotation of crews during Apollo, Cooper, Eisele and Mitchell would have flown on Apollo 13, but Cooper and Eisele never flew again: Deke Slayton, Director of Flight Crew Operations, felt that Cooper did not train as hard as he could have, while taking risks such as auto racing. Eisele was blackballed because of incidents during Apollo 7, which he had flown as CMP and which had seen conflict between the crew and ground controllers; he had also been involved in a messy divorce. Slayton only assigned the two as backups because he had few veteran astronauts available.[20] Mitchell escaped the fate of his crewmates, was assigned to the crew slated to fly Apollo 13, and when that crew was switched to Apollo 14 to give the mission commander, Alan Shepard more time to train, flew that mission as LMP, and walked on the Moon.[20]

For projects Mercury and Gemini, a prime and a backup crew had been designated, but for Apollo, a third group of astronauts, known as the support crew, was also designated. Slayton created the support crews early in the Apollo program on the advice of McDivitt, who would lead Apollo 9. McDivitt believed that, with preparation going on in facilities across the U.S., meetings that needed a member of the flight crew would be missed. Support crew members were to assist as directed by the mission commander.[21] Usually low in seniority, they assembled the mission's rules, flight plan, and checklists, and kept them updated.[22][23] For Apollo 10, they were: Joe Engle, James Irwin and Charles Duke.[24]

Flight directors were Gerry Griffin, Glynn Lunney, Milt Windler and Pete Frank.[25] Flight directors during Apollo had a one-sentence job description: "The flight director may take any actions necessary for crew safety and mission success."[26] CAPCOMs were Duke, Engle, Jack Lousma and Bruce McCandless II.[24]

En route to launch, Stafford touches a "Snoopy" doll

The command module was given the call sign "Charlie Brown" and the lunar module the call sign "Snoopy". These were taken from the characters in the comic strip, Peanuts, Charlie Brown and Snoopy.[24] These names were chosen by the astronauts with the approval of Charles Schulz, the strip's creator,[27] who was uncertain it was a good idea, since Charlie Brown was always a failure.[28] The choice of names was deemed undignified by some at NASA, as was the choice for Apollo 9's CM and LM ("Gumdrop" and "Spider"). Public relations chief Julian Scheer urged a change for the lunar landing mission.[29] But for Apollo 10, according to Cernan, "The P.R.-types lost this one big-time, for everybody on the planet knew the klutzy kid and his adventuresome beagle, and the names were embraced in a public relations bonanza."[30] Apollo 11's call signs were "Columbia" for the command module and "Eagle" for the lunar module.[31]

Snoopy, Charlie Brown's dog, was chosen for the call sign of the lunar module since it was to "snoop" around the landing site, with Charlie Brown given to the command module as Snoopy's companion.[32] Snoopy had been associated for some time with the space program, with workers who performed in an outstanding manner awarded silver "Snoopy pins", and Snoopy posters were seen at NASA facilities, with the cartoon dog having traded in his World War I aviator's headgear for a space helmet.[27] Stafford stated that, given the pins, "the choice of Snoopy [as call sign] was a way of acknowledging the contributions of the hundreds of thousands of people who got us there".[33] The use of the dog was also appropriate since in the comic strip, Snoopy had journeyed to the Moon the year before, thus defeating, according to Schulz, "the Americans, the Russians, and that stupid cat next door".[27]

Apollo 10 space-flown silver Robbins medallion

The shield-shaped mission insignia shows a large, three-dimensional Roman numeral X sitting on the Moon's surface, in Stafford's words, "to show that we had left our mark". Although it did not land on the Moon, the prominence of the number represents the significant contributions the mission made to the Apollo program. A CSM circles the Moon as an LM ascent stage flies up from its low pass over the lunar surface with its engine firing. The Earth is visible in the background. On the mission patch, a wide, light blue border carries the word APOLLO at the top and the crew names around the bottom. The patch is trimmed in gold. The insignia was designed by Allen Stevens of Rockwell International.[34]

Stafford (right) and Cernan in the lunar module simulator, April 1969

Apollo 10, the "F" mission or dress rehearsal for the lunar landing, had as its primary objectives to demonstrate crew, space vehicle and mission support facilities performance during a crewed mission to lunar orbit, and to evaluate the performance of the lunar module there. In addition, it was to attempt photography of Apollo Landing Site 2 (ALS-2) in the Sea of Tranquillity, the contemplated landing site for Apollo 11.[35] According to Stafford, "Our flight was to take the first lunar module to the moon. We would take the lunar module, go down to within about ten miles above the moon, nine miles above the mountains, radar map, photo map, pick out the first landing site, do the first rendezvous around the moon, pick out some future landing sites, and come home.[36]

Apollo 10 was to adhere as closely as possible to the plans for Apollo 11, including its trajectory to and from lunar orbit, the time line of events during the mission, and even the angle of the Sun at ALS-2. However, no landing was to be attempted.[37] ALS-1, given that number because it was the furthest to the east of the candidate sites,[lower-alpha 1] and also located in the Sea of Tranquility, had been extensively photographed by Apollo 8 astronauts; at the suggestion of scientist-astronaut Harrison Schmitt, the launch of Apollo 10 had been postponed a day so ALS-2 could be photographed under proper conditions. ALS-2 was chosen as the lunar landing site since it was relatively smooth, of scientific interest, and ALS-1 was deemed too far to the east.[38] Thus, when Apollo 10's launch date was announced on January 10, 1969, it was shifted from its placeholder date of May 1 to May 17, rather than to May 16. On March 17, 1969, the launch was slipped one day to May 18, to allow for a better view of ALS-3, to the west of ALS-2.[5] Another deviation from the plans for Apollo 11 was that Apollo 10 was to spend an additional day in lunar orbit once the CSM and LM rendezvoused; this was to allow time for additional testing of the LM's systems, as well as for photography of possible future Apollo landing sites.[39]

The Apollo 10 astronauts undertook five hours of formal training for each hour of the mission's eight-day duration. This was in addition to the normal mission preparations such as technical briefings, pilot meetings and study. They took part in the testing of the CSM at the Downey, California facility of its manufacturer, North American Rockwell, and of the LM at Grumman in Bethpage, New York. They visited Cambridge, Massachusetts for briefings on the Apollo Guidance Computer at the Massachusetts Institute of Technology Instrumentation Laboratory. They each spent more than 300 hours in simulators of the CM or LM at the Manned Spacecraft Center (MSC) in Houston and at Kennedy Space Center (KSC) in Florida. To train for the high-acceleration conditions they would experience in returning to Earth's atmosphere, they endured MSC's centrifuge.[40]

While Apollo 10 was meant to follow the procedures of a lunar landing mission to the point of powered descent, Apollo 10's LM was not capable of a landing and return to lunar orbit. The ascent stage was loaded with the amount of fuel and oxidizer it would have had remaining if it had lifted off from the surface and reached the altitude at which the Apollo 10 ascent stage fired; this was only about half the total amount required for lift off and rendezvous with the CSM. The mission-loaded LM weighed 13,941 kilograms (30,735 lb), compared to 15,095 kilograms (33,278 lb) for the Apollo 11 LM which made the first landing.[41] Additionally, the software necessary to guide the LM to a landing was not available at the time of Apollo 10.[8]

Craig Nelson wrote in his book Rocket Men that NASA took special precaution to ensure Stafford and Cernan would not attempt to make the first landing. Nelson quoted Cernan as saying "A lot of people thought about the kind of people we were: 'Don't give those guys an opportunity to land, 'cause they might!' So the ascent module, the part we lifted off the lunar surface with, was short-fueled. The fuel tanks weren't full. So had we literally tried to land on the Moon, we couldn't have gotten off."[44] Mueller, NASA's Associate Administrator for Manned Space Flight, stated, "There had been some speculation about whether or not the crew might have landed, having gotten so close. They might have wanted to, but it was impossible for that lunar module to land. It was an early design that was too heavy for a lunar landing, or, to be more precise, too heavy to be able to complete the ascent back to the command module. It was a test module, for the dress rehearsal only, and that was the way it was used."[45]

The descent stage of the LM was delivered to KSC on October 11, 1968, with the ascent stage arriving five days later. They were mated on November 2. The Service Module (SM) and Command Module (CM) arrived on November 24 and were mated two days later. Portions of the Saturn V launch vehicle arrived during November and December 1968, and the complete launch vehicle was erected in the Vehicle Assembly Building (VAB) on December 30. After being tested in an altitude chamber, the CSM was placed atop the launch vehicle on February 6, 1969.[46] The completed space vehicle was rolled out to Launch Complex 39B on March 11, 1969—the fact that it had been assembled in the VAB's High Bay 2 (the first time it had been used) required the crawler to exit the rear of the VAB before looping around the building and joining the main crawlerway, proceeding to the launch pad.[47] This rollout, using Mobile Launch Platform 3 (MLP-3),[5] happened eight days after the launch of Apollo 9, while that mission was still in orbit.[47]

The launch vehicle for Apollo 10 was a Saturn V, designated AS-505,[48] the fifth flight-ready Saturn V to be launched and the third to take astronauts to orbit.[49] The Saturn V differed from that used on Apollo 9 in having a lower dry weight (without propellant) in its first two stages, with a significant reduction to the interstage joining them. Although the S-IVB third stage was slightly heavier, all three stages could carry a greater weight of propellant, and the S-II second stage generated more thrust than that of Apollo 9.[50]

The Apollo spacecraft for the Apollo 10 mission was composed of Command Module 106 (CM-106), Service Module 106 (SM-106, together with the CM known as CSM-106), Lunar Module 4 (LM-4), a spacecraft-lunar module adapter (SLA), numbered as SLA-13A, and a launch escape system.[51][52] The SLA was a mating structure joining the Instrument Unit on the S-IVB stage of the Saturn V launch vehicle and the CSM, and acted as a housing for the LM, while the Launch Escape System (LES) contained rockets to propel the CM to safety if there was an aborted launch.[51] At about 133.8 metric tons, Apollo 10 would be the heaviest spacecraft to reach orbit to that point.[5]

Apollo 10 launched from KSC on May 18, 1969, at 12:49:00 EDT (16:49:00 UT), at the very start of a 4.5 hour launch window. The launch window was timed to secure optimal lighting conditions at Apollo Landing Site 2 at the time of the LM's closest approach to the site days later. The launch followed a countdown that had begun at 21:00:00 EDT on May 16 (01:00:00 UT on May 17). Apollo 10 launched from Pad 39B and was the only flight to launch from that pad during the Apollo program,[53] and it was also the only flight to be controlled from Firing Room 3 there.[8] Pad 39B was used because preparations for Apollo 11 had already begun at Pad 39A.[54]

Issues that arose during the countdown were dealt with during the built-in holds, and did not delay the mission.[24] On the day prior to launch, however, Cernan had been stopped for speeding while returning from a final visit with his wife and child. Lacking identification and under orders to tell no one who he was, Cernan later attested in his autobiography that he had feared being arrested. Launch pad leader Gunther Wendt, who had pulled over nearby after recognizing Cernan, explained the situation to the police officer, who then released Cernan despite the officer's skepticism that Cernan was an astronaut.[55]

Mission Control in Houston during an Apollo 10 telecast

The crew experienced a somewhat rough ride on the way to orbit due to pogo oscillations;[56] however, approximately twelve minutes after liftoff, the spacecraft successfully entered a low Earth orbit with a high point of 185.79 kilometers (100.32 nautical miles) and a low point of 184.66 kilometers (99.71 nautical miles).[57] All appeared to be normal during the systems review period in Earth orbit, and the crew restarted the S-IVB third stage to achieve trans-lunar injection (TLI) and send them towards the Moon. The vehicle shook again while executing the TLI burn, causing Cernan to be concerned that they might have to abort. However, the TLI burn was completed without incident.[58] Young then performed the transposition, docking, and extraction maneuver, separating the CSM from the S-IVB stage, turning around, and docking its nose to the top of the lunar module (LM), before separating from the S-IVB. Apollo 10 was the first mission to carry a color television camera inside the spacecraft, and mission controllers in Houston watched as Young performed the maneuver. Soon thereafter, the large television audience was treated to color views of the Earth.[59] One problem that was encountered was that the mylar cover of the CM's hatch had pulled loose, spilling quantities of fiberglass insulation into the tunnel, and then into both the CM and LM.[60] The S-IVB was fired by ground command and sent into solar orbit with a period of 344.88 days.[61]

The crew settled in for the voyage to the Moon. They had a light workload, and spent much of their time studying the flight plan or sleeping. They made five more television broadcasts back to Earth, and were informed that more than a billion people had watched some part of their activities.[62] In June 1969, the crew would accept a special Emmy Award on behalf of the first four Apollo crews for their television broadcasts from space.[63] One slight course correction was necessary;[62] this occurred at 26:32:56.8 into the mission and lasted 7.1 seconds. This aligned Apollo 10 with the trajectory Apollo 11 was expected to take.[61] One issue the crew encountered was bad-tasting food, as Stafford apparently used a double dose of chlorine in their drinking water, which had to be placed in their dehydrated food to reconstitute it.[5]

At 75:55:54 into the mission, 176.1 kilometers (95.1 nautical miles) above the far side of the Moon, the CSM's service propulsion system (SPS) engine was fired for 356.1 seconds to slow the spacecraft into a lunar orbit of 314.8 by 111.5 kilometers (170.0 by 60.2 nautical miles). This was followed, after two orbits of the Moon, with a 13.9 second firing of the SPS to circularize the orbit to 113.0 by 109.6 kilometers (61.0 by 59.2 nautical miles) at 80:25:08.1.[61] Within the first couple of hours after the initial lunar orbit insertion burn and following the circularization burn, the crew turned to tracking planned landmarks on the surface below to record observations and take photographs. In addition to ALS-1, ALS-2, and ALS-3, the crew of Apollo 10 observed and photographed a number of features on both the near and far sides of the Moon, including the craters Coriolis, King and Papaleksi.[64] Shortly after the circularization burn, the crew partook in a scheduled half-hour color television broadcast with descriptions and video transmissions of views of the lunar surface below.[65]

The LM crew, consisting of Stafford and Cernan, then prepared to enter the LM to check out its systems, which they did about an hour after the second burn.[61] When they entered Snoopy, they were met with a blizzard of fiberglass particles from the earlier problem, which they cleaned up with a vacuum as best they could. Stafford had to assist Cernan in removing smaller bits that had become caught in the latter's hair and eyebrows.[66] Stafford remembered that Cernan looked like he just came out of a chicken coop, and that the particles made them itch and got into the air conditioning system, and they were scraping it off the filter screens for the rest of the mission.[8] This was merely an annoyance, but the particles may have gotten into the docking ring joining the two craft and caused it to misalign slightly. Nevertheless, Mission Control determined that this was still within safe limits.[67]

Photograph of ALS-2 taken by Apollo 10

After Snoopy was checked out by Stafford and Cernan, they returned to Charlie Brown for a rest period. Then, Young remained in Charlie Brown while Stafford and Cernan re-entered Snoopy and undocked it from the CSM at 98:29:20.[65] Accordingly, Young became the first person to fly solo in lunar orbit.[68] Following the undocking, Stafford and Cernan deployed the LM's landing gear and inspected the LM's systems. The CSM performed an 8.3 second burn with its RCS thrusters to separate itself from the LM by about 30 feet, after which Young visually inspected the LM from the CSM. The CSM performed another separation burn, this time separating the two spacecraft by about 3.7 kilometers (2 nautical miles).[65] The LM crew thereafter performed the descent orbit insertion maneuver by firing their descent engine for 27.4 seconds at 99:46:01.6, and tested their craft's landing radar as they approached the 15,000-meter (50,000-foot) altitude where the subsequent Apollo 11 mission would begin powered descent to actually land on the Moon.[69] Previously, the LM's landing radar had only been tested under terrestrial conditions.[70] While the LM executed these maneuvers, Young monitored the location and status of the LM from the CSM, standing by to mount a rescue of the LM crew should it become necessary.[71] Cernan and Stafford surveyed ALS-2, coming within 14.4 kilometers (7.8 nautical miles) of the lunar surface at a point 15 degrees to its east, then performed a phasing burn at 100:58:25.93, thrusting for just under 40 seconds to allow a second pass at ALS-2.[69] Reporting on his observations of the site from the LM's low passes, Stafford indicated that ALS-2 seemed smoother than he had expected[71] and described its appearance as similar to the desert surrounding Blythe, California,[72] but that Apollo 11 could face rougher terrain downrange if it approached off-target.[71] Based upon Apollo 10's observations from relatively low altitude, NASA mission planners became comfortable enough with ALS-2 to confirm it as the target site for Apollo 11.[73]

LM Snoopy containing Stafford and Cernan, as inspected by Young after separation from Charlie Brown

The next action was to prepare to separate the LM ascent stage from the descent stage, to jettison the descent stage and fire the Ascent Propulsion System to return the ascent stage towards the CSM. As Stafford and Cernan prepared to do so, the LM began to gyrate out of control.[74] Alarmed, Cernan exclaimed into the hot mic being broadcast live, "Son of a bitch!", which, combined with other language used by the crew during the mission, generated some complaints back on Earth.[75] Stafford discarded the descent stage about five seconds after the tumbling began[65] and fought to regain control manually, suspecting that there might have been an "open thruster", or a thruster stuck firing,[76] and did so in time to be able to orient the spacecraft properly to send Snoopy to rejoin Charlie Brown.[74] The problem was traced to a switch controlling the mode of the abort guidance system; it was to be moved as part of the procedure, but each of the crew members switched it, thus returning it to the original position. Had they fired Snoopy in the wrong direction, they might have missed the rendezvous with Charlie Brown or crashed into the Moon at high speed.[77] Once Stafford had regained control of the LM ascent stage, which took about eight seconds,[74] the pair fired the ascent engine at the lowest point of the LM's orbit, mimicking the orbital insertion maneuver after launch from the lunar surface in a later landing mission. Snoopy coasted on that trajectory for about an hour before firing the engine once more to further fine-tune its approach to Charlie Brown.[65]

Snoopy successfully rendezvoused with and re-docked with Charlie Brown at 106:22:02, just under eight hours after undocking.[65] The docking was telecast live in color from the CSM.[78][79] After docking and once Cernan and Stafford had re-entered Charlie Brown, Snoopy was sealed-off and separated from Charlie Brown and Snoopy's ascent stage engine was fired to fuel depletion to send the ascent stage on a trajectory past the Moon and into a heliocentric orbit.[80][81] This maneuver was unlike the fate of the subsequent Apollo 11 ascent stage, which was left in lunar orbit to eventually crash (post-Apollo 11 ascent stages were steered into the Moon to obtain readings from seismometers placed on the surface, except for Apollo 13's ascent stage, which the crew used as a "life boat" to get safely back to Earth before releasing it to burn up in Earth's atmosphere, and Apollo 16's, which NASA lost control of after jettison).[81]

Post-splashdown crew recovery operations in the Pacific Ocean

Following ejection of the LM ascent stage, the crew slept and performed additional photography and observation of the lunar surface from orbit. Though the crew was able to locate 18 landmarks on the surface and take a number of additional photographs of various surface features, crew fatigue necessitated the cancellation of two scheduled television broadcasts. Thereafter, the main Service Propulsion System engine of the CSM re-ignited for about 2.5 minutes to set Apollo 10 on a trajectory towards Earth, achieving such a trajectory at 137:39:13.7. At the time of its departure from lunar orbit, Apollo 10 had orbited the Moon 31 times over the span of about 61 hours and 37 minutes.[65]

During the travel phase back to Earth, the crew performed some observational activities which included star-Earth horizon sightings for navigation. The crew also performed a scheduled test to gauge the reflectivity of the CSM's high gain antenna and broadcast six television transmissions of varying durations to show views inside the spacecraft and of the Earth and Moon from the crew's vantage point.[65] Cernan reported later that he and his crewmates became the first to "successfully shave in space" during the return trip, using a safety razor and thick shaving gel, as such items had been deemed a safety hazard and prohibited on earlier flights.[82] The crew fired the engine of the CSM for the only mid-course correction burn required during the return trip at 188:49:58, a few hours before separation of the CM from the SM. The burn lasted about 6.7 seconds.[65]

As the spacecraft rapidly approached Earth on the final day of the mission, Apollo 10 set the record for the fastest human spaceflight, traveling 39,897 km/h (11.08 km/s or 24,791 mph) relative to Earth, which is the fastest speed at which any humans have ever traveled.[83][84] This is because the return trajectory was designed to take only 42 hours rather than the normal 56.[85] In addition to that record, the Apollo 10 crew are the humans who have traveled the farthest away from their (Houston) homes, at a distance of 408,950 kilometers (220,820 nmi) (though the Apollo 13 crew was 200 km farther away from Earth as a whole).[86] While most Apollo missions orbited the Moon at the same 111 kilometers (60 nmi) from the lunar surface, the distance between the Earth and Moon varies by about 43,000 kilometers (23,000 nmi), between perigee and apogee, throughout each lunar month, and the Earth's rotation makes the distance to Houston vary by at most another 11,000 kilometers (5,900 nmi) each day. The Apollo 10 crew reached the farthest point in their orbit around the far side of the Moon at about the same time Earth's rotation put Houston nearly a full Earth diameter farther away.[87]

At 191:33:26, the CM (which contained the crew) separated from the SM in preparation for reentry, which occurred about fifteen minutes later at 191:48:54.5.[65] Splashdown of the CM occurred, approximately fifteen minutes after reentry, in the Pacific Ocean about 740 kilometres (400 nmi) east of American Samoa on May 26, 1969, at 16:52:23 UTC and mission elapsed time 192:03:23.[65] The astronauts were recovered by USS Princeton, onboard which they spent about four hours and took a congratulatory phone call from President Richard Nixon.[88] As they had not made contact with the lunar surface, Apollo 10's crew were not required to quarantine like the first landing crews would be.[89] They were flown to Pago Pago International Airport in Tafuna for a greeting reception, before boarding a C-141 cargo plane to Ellington Air Force Base near Houston.[88]