pictures courtesy NASA |
The Original Lunar Missions NASA Timetable Since Apollo 15
By November 1967, NASA released the planned schedule for the Apollo missions to be flown in 1968 and 1969, a combination of unmanned tests and manned flights on
both the Saturn 1B and Saturn 5 rockets, as the timetable was
highly dependent on the next to come Apollo 4 flight and the assumed success of all subsequent missions. The flights in 1968 would consist of:
The five following flights in 1969 were to be manned Saturn 5 missions, Apollo 11 through 15, with the first four as lunar mission development flights or lunar mission simulations. It was thought that a lunar landing could not be attempted before Apollo 15, or on one of the subsequent missions. The real Apollo missions flown were far from that timetable. Late, until into April 1968, it was far from certain whether the Moon landing goal would be met by the USA, or whether the Soviets might beat them. On April 27, 1968, NASA Administrator James E. Webb approved the plan to fly the third Saturn V mission with a crew as he based his decision on the work of engineers who quickly understood and fixed the problems encountered during the Apollo 6 mission earlier in that month and Webb decision brought the Moon landing closer
Selecting 5 Landing Sites
On February 8, 1968, after two years of study, NASA’s Apollo Site Selection Board announced five potential landing sites for the first human lunar landing. Five 3 by 5-mile landing areas, chosen from an original list of 30 candidate sites, satisfied certain criteria in which astronaut safety was paramount. All five sites were within the 'Apollo Zone of Interest,' a area on the visible side of the Moon between 45 degrees East and West longitude and between 5 degrees North and South of the lunar equator. To select the five areas, the Board used high-resolution orbital photography returned by five Lunar Orbiters and surface data and photographs provided by Surveyors that landed in the general area of some of the sites. The Board had considered the following criteria to determine the suitability of the candidate sites: smoothness, cleared approach paths, least amount of propellant needed, allowing for a delay in the launch countdown, remaining within reach 'free-return trajectory,' that is a path that would allow a coast around the Moon and safe return to Earth without any engine firings should a problem arise on the way to the Moon, a sufficient Sun angle for illumination (giving a one-day launch window per month), a slope of the terrain less than 2 degree. The five sites were sharing into two sites in the Sea of Tranquility, one in Sinus Medii, and two in the Ocean of Storms. When the first lunar landing closed in, the list was shortened to three sites before one of those would be designated as the prime landing site
->Abb.: C, commander; CM, Command module; CP, Command Module pilot; CSM, Command and Service Module; KSC, Kennedy Space Center (then Cape Canaveral), FL; LM, Lunar Module; LP, Lunar Module pilot; SPS, Service Propulsion System. note: the Apollo program had the commanders really piloting the LM and not the crewmember who officially wore the title 'LM pilot.' As Edwin Aldrin Jr was the LM Pilot for the Apollo 11 mission, it was Neil Armstrong who flew the LM
(data NASA)
Name | Launch | Landing | Crew | Mission | Duration |
---|---|---|---|---|---|
AS-201 | Feb 26th, 1966. Saturn 1B 11:12 a.m. EST. KSC (Complex 34) | Feb 26th, 1966 11:49 a.m. Atlantic Ocean | none | Suborbital Saturn launcher and launch loads test flight aboard the first Saturn IB launch vehicle developed by NASA's Marshall Space Flight Center (MSFC) to test the Saturn 1B launch vehicle and the Apollo Command and Service Modules. The objectives of the flight were to verify the structural integrity, launch loads, stage separation and operation of subsystems of the Saturn 1B, and evaluate the Apollo spacecraft subsystems, heatshield and mission support facilities. This was the first flight of the S-IB and S-IVB stages, including the first flight test of the liquid-hydrogen/liquid oxygen-propelled J-2 engine in the S-IVB stage. During the thirty-seven minute flight, the vehicle reached an altitude of 303 miles and traveled 5,264 miles downrange. Before, a number of flights of early elements of the Saturn V had occurred. The eighth Saturn flight -- the Saturn I Block II -- delivered into orbit by February 1965 the first of three Pegasus meteoroid detection satellites, aiming at comparing the performance of protected and unprotected solar cells, results of which informed future Apollo flights to the Moon. The Saturn I vehicle and its follow-on, the Saturn IB, served as test-bed rockets for the Saturn V | 36 mn 59 s |
AS-203 | July 5th, 1966. Saturn 1B 10:53 a.m. EDT. KSC (Complex 37-B) | no recovery | none | Saturn launcher second stage orbital test flight. 4 orbits performed. The second stage was the S-IVB, and the instrument unit of the Saturn V to obtain flight information under orbital conditions. The configuration of the Saturn IB was designed to match the Saturn V as closely as possible | 1h 28 mn 12s |
AS-202 | Aug 25th, 1966 1:15 p.m. EST. Saturn 1B. KSC (Complex 34) | Aug 25th, 1966 2:47 p.m. EST Pacific Ocean | unmanned | 3rd Saturn I and 2nd Command and Service Modules orbital test flight (CM heatshield test) | 1h 32 mn 54s |
AS-204 (Apollo 1) | - | - | Virgil Grissom/Edward White/Roger Chaffee | AS-204 was a launch pad test (Jan 27th, 1967). That mission was supposed to be the first crewed Apollo mission. A flash fire unluckily occurred killing all three crewmembers. Following the fire, the astronauts' widows requested that the mission be remembered as Apollo 1 and following missions would be numbered subsequently. The tragedy of Apollo 1 led to a 20-month halt in the program, and NASA engineers to redesign the spacecraft used for future Apollo missions. As a lesson learned, the cabin atmosphere of the Apollo 7 mission, during the countdown was maintained with a mixture of 65% oxygen and 35% nitrogen at sea level pressure. During the launch, the pressure was lowered to 5 pounds per square inch and the mixture adjusted to 100% oxygen. NASA implemented many other changes including an outward swiftly-opening unified Command Module hatch, a significant reduction in flammable materials in the cabin, improved spacesuits, a fire extinguishing system, and an emergency oxygen supply system in case the astronauts became separated from their suits. The agency also instituted improved training for emergency personnel | - |
non-flight Facility Verification Vehicle Saturn 500F | - | - | - | By 1966, the first Saturn V Moon rocket, a non-flight Facility Verification Vehicle called 500F was stacked in the Vehicle Assembly Building (VAB) and rolled out to the launch pad for fit checks. Three smaller Saturn 1B rockets had made unmanned test flights, two testing Apollo Command and Service Modules (CSM) during suborbital missions and the third testing the performance of the hydrogen tank in the booster’s upper stage, critical for understanding how that super-cold fuel behaves in weightlessness. Various stages of Saturn 500F began to arrive at the VAB in late 1965. Actual stacking of the vehicle on the Mobile Launch Platform began March 15, 1966, the first time a Saturn V was stacked in the VAB. A mockup of the Apollo CSM was used, and it along with the Spacecraft LM Adapter and the Launch Escape System (LES) was added to the booster on May 2, completing the first Saturn V stack. By June 8, Hurricane Alma forced NASA to roll 500F back to the VAB as it was rolled again after two days. Meanwhile, at the nearby CCAFS, two Saturn 1Bs were being readied for flight. So between May 25 and July 5, three Saturn rockets stood on their respective launch pads, as unfortunately, no photographs have been found documenting this historic occurrence. On October 14th, 1966, the Saturn 500F was eventually rolled back for destacking as a improvised shake text occurred before. By pushing and pulling the rocket a group of engineers got the rocket swaying at its natural frequency, providing for the vibrations (the LES fell on one of the work platforms with fortunately no injuries nor significant damage). That first test on the pad proved sufficient as not other test was scheduled further, and the destacking process occurred. Workers in the VAB then passed to stacking the Saturn 501, to complete the first successful flight of a Saturn V during the unmanned Apollo 4 mission. By March 1967, the AS-500D configuration I testing ended with a special test to verify the flight control system. The test program included roll, pitch, yaw and longitudinal testing, completed earlier in 1967. AS-500D was a dynamic test article of the Saturn V space vehicle | - |
Apollo 4 (or AS-501) | Nov 9th, 1967. Saturn V 7:00 a.m. EST. KSC (Complex 39-A) | Nov 9th, 1967 3:37 p.m. EST Atlantic Ocean | unmanned | First Saturn V launcher and CSM orbital test flight. The Apollo 4 mission was the first all-up test of the Saturn V rocket, designed to test all aspects of the Saturn V launch vehicle. Mission objectives included testing of structural integrity, compatibility of launch vehicle and spacecraft, heat shield and thermal seal integrity, overall reentry operations, launch loads and dynamic characteristics, stage separation, launch vehicle subsystems, the emergency detection system, and mission support facilities and operations. The mission was deemed a successful test. Apollo 4, 5, and 6 practiced some of the maneuvers necessary to build up to a lunar landing, such as the first flight of the Saturn V rocket and high-speed reentry. Apollo 2 and 3 were skipped in the sequence out of respect to the Apollo 1 crew. Third (S-IVB) stage re-ignition, S-IVB-CSM separation, SPS ignitions, Command module-Service module separation. The Saturn V rocket for the uncrewed Apollo 4 mission was the first launcher stacked in the Vehicle Assembly Building, or VAB, the first operational Saturn V, and the first to lift from launch pad 39-A at the Kennedy Space Center. Apollo 4's rollout began early on Aug. 26, 1967. All the elements of a Apollo flight had been reunited for the first time. From a nearly circular 115-mile orbit, the S-IVB's put the spacecraft into an elliptical orbit with a apogee of 11,200 miles; then the command module propulsion system fired to reach a speed of 24,900 mph, simulating a return from the Moon. That first flight lasted almost nine hours. Landing 9.9 miles from targeted landing point in the Pacific Ocean. The stack underwent a series of tests, and one of the most important was the Count Down Demonstration Test (CDDT), with the vehicle powered up and fully fueled. It began September 27 and planned to last six days as many unforeseen technical challenges brought the delay to 17 days. Getting Apollo 4 and its Saturn 5 ready for flight was a important milestone on the way to landing men on the Moon as it was the sign that the U.S.A. were back on track to land on the Moon following the Apollo 1 fire earlier in 1967. The countdown lasted three days. Scientists calculated that the noise created by the launch was one of the loudest natural or man-made ever as the vibrations rattled the press site several miles away. President Lyndon B. Johnson said of the flight: 'The whole world could see the awesome sight of the first launch of what is now the largest rocket ever flown. This launching symbolizes the power this nation is harnessing for the peaceful exploration of space.' | 8h 36mn 59s |
Apollo 5 | Jan 22nd, 1968. Saturn 1B. 5:48 p.m.EST. KSC (Complex 37-B) | none | unmanned | First Lunar Module test flight and evaluation of the S-IVB stage instrument performance, as the S-IVB was to serve as the second stage on Apollo 5's launch vehicle, the Saturn IB. LM descent and ascent engines orbital tests. The strength of the LM overall structure also was tested. The ascent engine was ignited successfully simulating an abort during the landing phase. This involved the ascent propulsion system being started simultaneously with the descent engine being shut down. Maj. Gen. Samuel Philips, director of the Apollo Program Office, said that the lunar module's maiden flight completed testing of the last major piece of Apollo flight hardware as all other Apollo hardware elements had been tested throughout the previous two years. The Apollo 5 mission was launched atop a Saturn 1B rocket. The Lunar Module (LM) was built by the Grumman Corporation. The test LM-1 was not planned to land anywhere and didn’t carry any landing legs which save weight. During the 11-hour flight test of the LEM, a malfunction occurred because the guidance computer terminated the planned initial 39-second firing of the descent stage engine after only 4 seconds and the crew and Houston passed to fire the descent engine manually. The LM-1 also simulated a aborted landing, the so-called 'fire-in-the-hole' staging, and again for more than six minutes until the fuel was depleted. Since the LM was not designed to return to Earth, both stages burned up in the atmosphere upon reentry. The next time a LM would fly in space, it would carry astronauts as the Saturn 1B was deemed so reliable that its next launch would carry a crew to test the Apollo Command and Service Module in Earth orbit. This was the first significant change to the Apollo Program plan that NASA announced in November 1967 and brought the Agency one step closer to a Moon landing. For many Americans, on the other hand, the Apollo 5 mission was overshadowed by two major breaking news events unfolding halfway around the world. The day the Apollo 5 mission ended, North Korea seized the USS Pueblo and its crew and held them captive for 11 months as, a week after Apollo 5, Americans were shocked by the ferocity of the Tet Offensive in Vietnam, a escalation of that conflict | 11h 10 mn (time in orbit only) |
Apollo 6 | April 4th, 1968. Saturn V. 7:00 a.m. EST. KSC (Complex 39-A) | April 4th, 1968 5:23 p.m. EST Atlantic Ocean | unmanned | That mission represented the Saturn V rocket on its second flight, along with the Apollo spacecraft. No active LM was carried on this flight, replaced instead with the LM Test Article (LTA) 2R to partially simulate its mass in order to approximate structural loads on the rocket during launch. The primary objectives of the mission were to demonstrate structural and thermal integrity and compatibility of the launch vehicle and spacecraft, confirm launch loads and dynamic characteristics, and verify stage separations, propulsion, guidance and control, electrical systems, emergency detection system, and mission support facilities and operations, including Command Module recovery. The plan was for the first three stages to place the spacecraft still attached to the third stage into low Earth orbit and then, to simulate a Translunar Injection (TLI), the third stage reigniting to send the spacecraft into a highly elliptical Earth orbit. Soon after TLI, the Service Module (SM) engine would fire to slow the spacecraft down in a simulation of a direct-return abort, with Apollo 6 reaching an altitude of about 14,000 miles before descending back toward Earth. The SM engine would fire again to increase the spacecraft’s speed on reentry to about 25,000 miles per hour to mimic a lunar return, much as happened on Apollo 4. The mission however ran into trouble from the start. Two minutes into the flight, the first stage experienced about 30 seconds of vertical oscillations known as the 'pogo effect,' which caused no serious damage but would have been very uncomfortable for any crew. Then during the second stage burn, two of the five engines shut down prematurely. The remaining three engines burned longer to compensate for the reduced thrust, as did the third stage to propel Apollo 6 into orbit. When it was time for the third stage to restart, it simply wouldn’t. The flight control team then decided on an alternate mission plan to separate the spacecraft from the third stage and use the SM engine instead to reach the nearly 14,000-mile altitude. But this used so much fuel that the second SM burn could not be carried out, so reentry occurred at less than the planned speed. Apollo 6 splashed down in the Pacific Ocean after a troubled flight of 9 hours and 57 minutes and was recovered aboard the aircraft carrier USS Okinawa by some 49.7 miles off target. The rocket problems notwithstanding, on the other hand, Apollo 6 returned some stunning photographic results. Camera pods in the second stage that were jettisoned and recovered after launch recorded some stunning film of the first stage separation, imagery that has become iconic of Saturn V launches (and often incorrectly attributed to Apollo 11). While Apollo 6 was orbiting the Earth, the spacecraft's special 70-millimeter camera obtained some spectacular color stereo photographs. These were later found to be excellent for cartographic, topographic, and geographic studies of continental areas, coastal regions, and shallow waters. The camera had a haze-penetrating film and filter combination that provided better color balance and higher resolution than any photographs obtained during the Mercury and Gemini flights. Apollo 6 at last, did not garner much press attention as major events in the country overshadowed the mission like the presidential elections President Lyndon B. Johnson announced he would not run or the assassination of civil rights leader Rev. Martin Luther King. After detailed analysis of the Saturn V flight by engineers at Marshall Space Flight Center, NASA managers decided they could solve the pogo issue and the engine malfunctions and that another unmanned test flight was not necessary, bringing to that the next Saturn V launch would carry a crew! | 10h 22mn 59s |
->The Pogo Effect and Other Troubles With the Apollo 6 Mission
Pogo occurred when a
partial vacuum in the fuel and oxidizer feed lines reached the engine firing
chamber causing the engine to skip. These oscillations then travelled up the
axis of the launch vehicle resulting in intense vibration in the Command and
Service Module (CSM) and causing some structural damage. The pogo problem was nothing new to the world of rocketry as early launch
vehicles such as the Thor, and even the Titan II used for the Gemini program,
had a similar experience, as did, to a lesser degree, the Apollo 4 mission. Marshall Space Flight Center Director Wernher von Braun conceded that the 'flight clearly left a lot to be desired. With [this problem], we just cannot go to the Moon,' as the perspective to place a crew on Apollo 8 made solving the pogo issue of a critical importance. NASA formed a Pogo Working Group comprised of more than a 1,000 government and
industry engineers to come up with a solution capable of verification through
ground testing. The Working Group organized a rigorous investigation, which
determined the key to mitigating the pogo effect included ‘de-tuning’ the F-1
engine to change the frequency of the vibration it produced and filling the
charged prevalve cavities on the liquid oxygen (LOX) feed lines with helium gas
from the tank pressurization system. Injecting helium into those lines prior to
ignition would effectively work as a shock absorber by holding engine pulses
into LOX lines and the vehicle structure preventing the oscillations from
traveling up and down fuel and oxidizer feed lines. Mathematical models were developed based upon previous flights and verified
through a series of tests, while static test firings of first stages for
upcoming missions were tested with pogo suppression hardware installed as, on July 15, Apollo Program Director and NASA Associate Administrator for Manned Space Flight concurred with the group’s solution. The Pogo oscillation problems also affected the stacking of the Apollo 8, bringing to a de-stacking and repairs. However, the failure of the J-2 engines on the second and third stages presented
more of a challenge. Early on, the team investigating the failure discovered a
leak of liquid hydrogen gas at 70 seconds into the burning of the second stage
in engine number 2. This leak in the bellows section of the Augmented Spark
Ignitor (ASI) fuel line started as a small leak in a defect which eventually
resulted in catastrophic failure. The investigation determined that
unfortunately, the failure of engine two was compounded when, as combustion
pressure began to fall, sensing equipment triggered the shutdown of a different
engine, number three. The restart failure of the J-2 engine in the third stage
was chalked up to the same defect in the ASI. How was such a major problem missed by engineers during testing? It turns out
that during ground testing, frost on the lines from cold propellant temperatures
had added a degree of extra protection from vibrations in the bellows section.
Because this same process does not occur in the vacuum of space, fatigue cracks
emerged. Vacuum tests of eight ASI lines at Rocketdyne facilities resulted in
the failure of all eight, each time in the same bellows section. The fix
required the removal of the bellows sections from subsequent lines and
additional vacuum testing on all upper second and third stage engine flexible
lines. Almost two years of Apollo spacecraft redesign and testing occurred, generally, after the Apollo 1 fire in January 1967
->August 1968 NASA Decisions
In August 1968, Apollo Spacecraft Program Manager faced that the Saturn V rocket performed extremely well on Apollo 4, its
first test flight in November 1967, but during Apollo 6 five months later, it
encountered several significant anomalies. Engineers found solutions to those
problems and NASA management decided that on its third flight, Apollo 8,
expected to occur before the end of the year, the Saturn V would carry
astronauts. As the Apollo Command and Service Module (CSM) had performed well and was ready for
its first crewed Earth orbital shakedown mission, Apollo 7, in October, the
Lunar Module (LM) as far as it is concerned, performed well on Apollo 5, its first uncrewed
flight in January 1968. The LM that would first carry astronauts arrived at
Kennedy Space Center in June. But testing revealed numerous problems with the
vehicle that indicated it wouldn’t be ready to fly until sometime in early 1969. Apollo 8 by late 1967, was considered to be the third uncrewed test flight of the Moon rocket as NASA in April 1968, transformed it into the first Saturn V to carry a crew and to test the Lunar Module (LM) and the Command and Service Module (CSM), in an Earth orbital flight. Preparations for the LM ran behind schedule, and in August NASA deleted that component from the mission and began to consider other options, including a lunar orbital flight. A final decision on a lunar mission was contingent upon Apollo 7 being successful. Deletion of the LM from the flight also led to a change of the crew who would fly Apollo 8. To complicate matters, intelligence reports
indicated that the Soviets were close to sending cosmonauts on a trip around the
Moon, possibly before the end of the year. In a meeting with other managers, the Apollo Spacecraft Program Manager exposed his proposal of sending Apollo 8 to the Moon, instead of an Earth orbital test of the
LM. His rationale was that since the LM wouldn’t be ready before early 1969, to
maintain the program’s momentum, a flight was needed to fill the gap after
Apollo 7. Without a LM, another Earth orbital flight wouldn’t advance the
program much. However, by sending Apollo 8 to the Moon NASA would gain valuable
experience in navigation and communications at lunar distances. The plan was eventually approved by all NASA centers involved and NASA's chain of decision and the Apollo 9 planned crew swapped roles with the Apollo 8's. Apollo 8 was to fly on a circumlunar mission
without a LM in December 1968 and the originally assigned Apollo 8 team of
Commander James A. McDivitt, David R. Scott and Russell L. Schweickart
would instead fly the Apollo 9 Earth orbital first LM test in early 1969. Assuming NASA directors, and ultimately President Lyndon B. Johnson agreed to the
plan, NASA had only four months to prepare for the first human voyage to another
celestial body. No formal decision about a lunar mission eventually would be made until after a successful Apollo 7 flight in October 1968, which would prove the space-worthiness of the Apollo Command and Service Module in Earth orbit. Until then, plans for a lunar mission were kept strictly within NASA. A formal announcement on August 19 stated only that the LM was no longer part of the Apollo 8 flight and that the agency was considering various mission objectives. Following tests in 1968, NASA engineers modified the spacecraft, included replacing the older version side hatch
with an easier to open unified lightweight version, installing a docking probe
to the forward tunnel to dock with the
Lunar Module, and installing a high-gain steerable antenna needed for
communications at lunar distances. Other changes were applied too in lesser equipments and procedures. The preparing of the Apollo 7 was also marked by that NASA Administrator James E. Webb unexpectedly announced that he would be resigning effective October 7, his 62nd birthday. In September 1968, NASA had also began preparing for the next two missions following Apollo 7, which were to use the larger Saturn V rocket to carry astronauts into space. Apollo 8, scheduled for December 1968, was at this time planned as an Earth orbital test of the Saturn V with the Command and Service Module (CSM), but NASA was considering other options for the mission, including a circumlunar flight as its objective was still under consideration, dependent on the success of Apollo 7. Apollo 9 was planned for early 1969 to be the first crewed flight of a Lunar Module (LM), in an Earth orbit test of all three principal Apollo spacecraft components. And Soviet pressure only increased through the fall as they
flew two uncrewed Zond circumlunar missions, and US reconnaissance satellite
imagery showed a large Saturn V-sized N-1 rocket undergoing testing on its
launch pad at the Baykonur Cosmodrome in Kazakhstan. The context thus was that of that the race to the Moon was heating up between the
United States and the Soviet Union. Both powers were also recovering from tragic losses. Three Apollo 1 astronauts
perished in a launch pad fire on Jan. 27, 1967 as that same year, a lone
cosmonaut aboard Soyuz 1 died when the spacecraft crashed on April 24. Russia also made strides with that problem as cosmonaut Georgi T. Beregovoy's successful flight also added to pressure on NASA. With all this work to prepare for challenging space flights, NASA employees took some time out to celebrate the Agency's 10th anniversary on October 1. Several centers held open houses to commemorate the event. By October 8th, 1968, both the Apollo 7 and 8 missions were standing at their respective launch pad in the KSC, Complex 34 (along Cape Canaveral shores) and 39-A (one of both main pads of the KSC still used nowadays) respectively, and the preparation of the Apollo 8 mission kept there until launch. The NASA announced that the Apollo 8 mission would be a orbital flight around the Moon on November 12, 1968. Instead of delaying Apollo 8 for cause of that the Lunar Module could not be ready in time, NASA turned the Apollo 8 into acquiring valuable experience in navigation and communications at lunar distances. The flight plan for Apollo 8 called for a open-ended mission using commit points to advance to each successive goal. The crew assigned to the Apollo 8 mission, Commander Frank Borman, Command Module Pilot James A. Lovell, and Lunar Module Pilot William A. Anders, held a news conference in the auditorium at the Manned Spacecraft Center, now the Johnson Space Center in Houston, on November 16
Apollo 7 | Oct 11th, 1968. Saturn 1B. 11:02 a.m. EDT. KSC (Complex 34) | Oct 22nd, 1968 7:11 p.m. EDT Atlantic Ocean | Donn Eisele, Walt Cunningham, Walter Schira (C) | Manned Command and Service Module test mission (SPS included). The Apollo 7 was the first American crewed flight since Gemini 12 in November 1966, and marked a resumption of human space flights halted by the Apollo fire in January 1967. Senior management from NASA Headquarters, the Kennedy Space Center (KSC), the Marshall Space Flight Center, and the Manned Spacecraft Center (now the Johnson Space Center) met at KSC on October 3 for the Apollo 7 Flight Readiness Review and gave the green light to the flight. That first crewed Apollo space mission was an engineering test flight, with its primary objectives to demonstrate the command and service module, or CSM, CSM rendezvous capability, crew performance and mission support facilities performance during a crewed mission. It was the first time astronauts flew aboard a Saturn V in its Saturn IB version. It was also the first U.S. three-person spaceflight and the first time astronauts were launched by a liquid hydrogen-powered rocket. Donn Eisele and Walt Cunningham belonged to NASA's 3rd class of astronauts as they flew for the first time. Apollo 7 was nicknamed 'The Walt, Wally and Donn Show,' from the names of crew. The flight was designated as open-ended depending on its progress in orbit but was expected to last 10.8 days, long enough to prove the spacecraft’s ability to carry out a lunar mission. The flight proper was preceded with a series of tests. The Command and Service Module was assembled with the Saturn IB launcher at the pad only. As one of the tests to certify Apollo 7 to carry out the first crewed Apollo mission, three astronauts participated in a 48-hour recovery test of an Apollo Command Module (CM) at sea, in the Gulf of Mexico. The test also checked how a Apollo spacecraft fared if the recovery of the capsule and crew were delayed for up to two days. The crew reported that while they did not 'recommend the Apollo spacecraft for any extended sea voyages' they encountered no serious habitability problems during the 48-hour test. The Apollo capsule used in this recovery test, CM-007A, served primarily as a module for crewed post landing tests as its instrument panel was just a mockup. Astronauts practiced escape exercises. A 6-day Countdown Demonstration Test (CDDT) also occurred a complete rehearsal of the actual countdown to exercise not only the launch team at KSC but also Mission Control at the Manned Spacecraft Center (controllers monitored the simulated countdown in the firing room of Launch Complex 34, in the reinforced concrete Blockhouse about 320 yards from the launch pad). Schirra reported the ascent to orbit was smooth, and smoother than his previous launches on Atlas and Titan rockets. About 15 hours into the mission Schirra reported that he had come down with a head cold as both other astronauts reported soon similar symptoms as headward shift of body fluids in space aggravated the congestion which remained for the rest of the mission, likely contributing to some of the tensions between them and Mission Control (that lately brought that crew flew the reentry into the Earth's atmosphere without their helmets to be able to accomodate with pressure increase, which the Mission Control reluctantly agreed). Crew flew 163 orbits as the mission scored a total flight time of 260 hours and 9 minutes, and TV broadcasted live. A simulated LM docking was performed using the spent S-IVB stage. The CSM SPS engine was used to slow Apollo for reentry on its Earth's orbit as 8 test-firings of the engine occurred flawlessly, giving the crew a real kick! Broadcasting live television from the spacecraft, the first television broadcast from inside an American spacecraft, consisted in that, three days after liftoff, the Apollo 7 camera was turned on, allowing Mission Control and viewers around the world to watch the crew in orbit. Eisele holded a sign which said 'From the lovely Apollo room, high atop everything, or 'Keep Those Cards and Letters Coming In, Folks.' Seven TV events occurred in total as they had to be timed with spacecraft passes over the continental United States, because only the ground stations in Corpus Christi, Texas, and Merritt Island, Florida, had the equipment to receive the signals and convert them into the proper format for broadcasting. In 1969 the Apollo 7 crew received a special Emmy Award from the National Academy of Television Arts and Sciences for their TV broadcasts from space. One notable event that took place while they were in space was the wedding of Jacqueline Kennedy, widow of President John F. Kennedy, to Greek tycoon Aristotle Onassis. For the first time, the crew could have hot meals including coffee available to them, using heated water to rehydrate packages of food, marking a significant improvement over earlier programs. To stay fit, astronauts spent time working out on a portable exercise device called the Exer-Genie. After the flight, Schirra described the Apollo CSM as 'a magnificent flying machine.' The flight generally, was so succesfull that Lt. Gen. Samuel C. Phillips, director of NASA's Apollo Program Office declared that Apollo 7 'accomplished 101%' of its planned objectives and that he considered that he had 'every confidence that the progress of this mission will let us accomplish [a lunar landing] by the end of next year,' as that much work still remained before NASA decided to send Apollo 8 on a lunar orbit mission. Mission landed southeast of Bermuda, less than 1.2 mile off target landing point. In support of Apollo 7, the first manned Apollo mission planned for October 1968, and other future missions, engineers needed to certify the Command and Service Module (CSM) to carry a crew. Part of that certification included conducting structural tests of the vehicle so it is not impaired by severe launch environments or the aerodynamic noise and vibration stresses expected during flight. The lunar mission vibration criteria were also verified. A manned test on February 10, 1968 was performed with Astronaut Gordon Cooper aboard Apollo CSM 105 and two mannequins to determine if crewmen would experience visual problems during the Saturn V launch low-frequency vibrations. Eventually only a bent strut in the vehicle was found like a default at that strut’s installation procedures were modified to prevent a recurrence during an actual flight. Apollo 7 became the second longest American spaceflight, a position it held until Apollo 15 in 1971 as the mission also passed the expected duration of a lunar landing mission, proving that the Apollo spacecraft and its crew could operate successfully for that length of time | 10d 20h 9mn | ||
Apollo 8 | Dec 21st, 1968. Saturn V. 7:51 a.m. EST. KSC (Complex 39-A) | Dec 27th, 1968 10:51 a.m. EST Pacific Ocean | Frank Borman, James Lovell Jr., William Anders |
| 6d 3h 0mn 42s | ||
Apollo 9 | March 3rd, 1969. Saturn V. 11:00 a.m. EST. KSC (Complex 39-A) | March 13th, 1969 12:00 p.m. EST Atlantic Ocean | James McDivitt, David Scott, Russell Schweickart | Earth orbit manned Lunar Module test flight (rendez-vous, docking, separation). Stacking of the Apollo 9 Saturn V was completed in October 1968, with the Apollo spacecraft added in early December as that mission was the first crewed mission to test the all-important LM. As three crew developed sore throats and nasal congestion the launch countdown had to be halted. The most critical tasks were scheduled for the first five days of the mission to maximize the chances of accomplishing them, should a anomaly force an early end to the flight. The crew had to conduct the first extravehicular activity of the Apollo program, the only one scheduled before the spacewalk on the Moon’s surface, to test the reliability of the Apollo A-7L space suit and the Portable Life Support System (PLSS) backpack. Astronauts were also to test the capability of crews to transfer through open space, in case a malfunction with the transfer tunnel or hatches between the two spacecraft prevented an internal transfer. This was the only spacewalk experience and in-orbit vacuum test of the space suit before the Moon landing. 2 versions of the Apollo A7L space suit had been developped -- one for intravehicular activity (IVA), with a hose porting life support -- and one for extravehicular activity (EVA) which included the Portable Life Support System (PLSS) backpack. On its first uncrewed test flight, with Apollo 5 in January 1968, the LM had performed so well that NASA deemed a second unpiloted test flight unnecessary. The mission was designed to rehearse all the steps and reproduce all the events of the Apollo 11 mission with the exception of the lunar touchdown, stay and liftoff. It had to perform a engineering test of the lunar module and overall check of the launch vehicle and spacecraft systems, the crew, and procedures as all the objectives were successfully met. Apollo 9 was the second crewed mission to launch on a Saturn V rocket. Primary mission objectives included an Earth-orbital engineering test of the first crewed LM and an overall checkout of the launch vehicle and spacecraft systems, the crew and procedures. All prime mission objectives were met and all major spacecraft systems were successfully demonstrated. The Apollo 9 spacecraft, still attached to the S-IVB third stage was placed into a accurate orbit just over 11 minutes after liftoff as it was the heaviest crewed spacecraft placed into Earth orbit to that time, at 95,231 pounds. After launch, control passed from the Launch Control Center (LCC) to Mission Control at the Manned Spacecraft Center, now the Johnson Space Center in Houston where three teams of controllers worked in eight-hour shifts until splashdown. Three capsule communicators, or Capcoms, astronauts in Mission Control speaking directly with the crew succeded themselves during the mission. Two hours and 41 minutes after launch, the Command and Service Module separated from the S-IVB third stage and pulled a safe distance away and the four panels of the Spacecraft LM Adapter (SLA) that protected the LM during launch were jettisoned. The Apollo capsule was turned around to face the LM still attached to the S-IVB, and slowly closed the gap between the two spacecraft, completing a successful docking. About an hour later, springs ejected the docked spacecraft from the S-IVB. Ground controllers also took benefit from the flight as they twice restarted the S-IVB’s engine to simulate a Trans Lunar Injection, eventually sending the spent rocket stage into solar orbit. Then several engine burns proved the the controllability of the docked LM and CSM vehicles. Astronauts then entered into the LM and activated varied systems of which the engine of its Descent Propulsion System (DPS). Astronaut Schweickart experienced symptoms of space motion sickness. The main purpose of testing the LM engine was paradoxically to evaluate if it could serve as a backup in case of a problem with the Apollo capsule's Service Propulsion System (SPS)! On Flight Day 4, a spacewalk occurred out of both the Command Module and the LM, with a umbilical link or a life support system respectively. On Flight Day 5, flight tests were performed related to the LM's maneuvrability and to rendezvous with the CSM (the LM was brought up to a distance of 100 miles away), during which the LM's Descent Stage was jettisoned. After a successful rendezvous maneuver, astronauts jettisoned the LM. The crew then put to work Experiment S065 Multispectral Terrain Photography, a cluster of four Hasselblad 70 mm cameras pointed out the Command Module’s (CM) round hatch window, taking photographs simultaneously in four specific portions of the visible and near infrared spectrum. The experiment served as a precursor for the Earth Resources Technology Satellite (ERTS), later renamed Landsat, and for multispectral photography conducted aboard the Skylab space station in the early 1970's. Mission control decided to delay mission's splashdown by one day due to inclement weather at the planned time. A 11-second engine burn over Hawaii deorbited the crew. The capsule then separated from the service module and pointed its heat shield in the direction of reentry, with a 4-minute radio blackout occurring in the atmospheric layers. The capsule touched down 3 miles from the prime recovery USS Guadalcanal. The Apollo capsule was transported to North American Rockwell for postflight inspection. NASA also took profit of the return of Apollo to conduct a simulation of the whole recovery operations, of which the Mobile Quarantine Facility (MQF), with the Lunar Receiving Laboratory. 'We tested every possible thing that could be tested [in Earth's orbit],' one of the crew said | 10d 1h | ||
Apollo 10 | May 18th, 1969. Saturn V. 12:49 a.m. EDT. KSC (Complex 39-B) | May 29th, 1969 12:52 p.m. EDT. Pacific Ocean | Eugene Cernan, John Young, Thomas Stafford | The crew for the Apollo 10 mission, scheduled for the spring of 1969, had been announced on Nov. 13, 1968. Possible scenarios for Apollo 10 ranged from an Earth orbital flight to a lunar orbit mission, depending on the success of the preceding two missions. On Mar. 11, 1969, NASA rolled the Saturn V rocket for the Apollo 10 mission to Launch Pad 39B at Kennedy Space Center marking the first use of the second pad at Launch Complex 39. The assembly of the Apollo 10 Saturn V had taken place in the VAB’s High Bay 2, which required the rollout to occur from the rear of the building, loop around to the front and then make a left turn to reach Launch Pad B. The eight-day Apollo 10 mission, targeting a mid-May launch, was planned as a dress rehearsal of the Moon landing. The LM was to descend to about 50,000 feet above the lunar surface, and photograph the primary landing site for Apollo 11 in the Sea of Tranquility as except for the actual descent and touchdown to the surface, Apollo 10 would follow all the steps of the actual Moon landing mission. Stafford stated before the mission that Apollo 10 was to 'sort out all the unknowns and actually pave the whole way for the lunar landing mission.' Apollo 10 Command Module was featured with a color TV system in addition to the standard black and white cameras (color television broadcasts throughout the flight brought the experience into everyone's living rooms). A Flight Readiness Test (FRT) occurred April 7-10 1969 and followed by the Countdown Demonstration Test in early May. The crew also participated in simulations of the various phases of their mission, a water egress after splashdown training in the Gulf of Mexico. Apollo 10 eventually was a Moon rehearsal flight (first comprehensive lunar-orbital qualification and verification test of the lunar lander altogether with testing the work of flight controllers and control network). All operations were performed except real landing (on May, 22nd Stafford and Cernan entered LM and practised low lunar orbit passes as Young kept orbiting the Moon a an altitude of 60 miles. They descended down to 47,400 feet from surface during an 8-h flight; the crew also refined knowledge of the lunar gravity needed to calibrate the descent guidance system for a landing). 31 lunar orbits. TV images transmitted Earth as photographs were taken from the Apollo 11 landing site in the Sea of Tranquility. That flight was the first to make use of Launch Pad 39B as Apollo 10 set the record for the highest velocity attained to date by a piloted vehicle at 24,791 mph during reentry, and still holding as the capsule was descending to the Entry Interface. Apollo 11 first was placed into a 69- by 196-mile elliptical orbit around the Moon, then circularized at 69 miles, as Stafford radioed to Mission Control: 'You can tell the world that we have arrived,' as Cernan summing the lunar views the crew saw below them: 'It might sound corny, but the view is really out of this world.' They also saw how many features were lighted by Earthshine on the dark side of the Moon. During its 8-hour 10-minute solo flight the Snoopy LM met all planned objectives. Due to residual air pressure in the docking tunnel that couldn't be vented, Snoopy departed at a higher than expected speed as a fired engine sent it into a solar orbit after docking back. During their last day in lunar orbit, Stafford, Cernan, and Young took stereo images of the Apollo 11 landing site and treated the ground to a 24-minute color TV broadcast, showing views of the lunar surface including that landing site. The Trans Earth Injection (TEI), a 165-second burn of the Service Propulsion System (SPS) engine was successfully completed while the spacecraft was behind the Moon and out of communications with Earth. The TEI burn was so precise that the first planned midcourse correction during the coast to Earth was not needed. The crew conducted a small midcourse correction maneuver near Earth only, refining the path to reentry and Apollo 10 splashed down East of American Samoa, shortly before sunrise | 8d 0h 3mn 23s | ||
Apollo 11 | July 16th, 1969. Saturn V. 9:32 a.m. EDT KSC (Complex 39-A) | July 24th, 1969 12:50 p.m. EDT Pacific Ocean | Neil Armstrong (C), Michael Collins (CP), Edwin Aldrin Jr (LP) | Landing mission. On March 5, 1969 U.S. President Richard M. Nixon had nominated Thomas O. Paine, Acting NASA Administrator since October 1968, to be NASA’s third Administrator as March 28, the USA learned of the death of former President Dwight D. Eisenhower, who had been instrumental in the establishment of NASA in 1958. The primary goal of the first Moon landing mission was still a goal of advancing lunar space flight, in demonstrating that the Apollo spacecraft systems could safely land two astronauts on the surface and return them safely to Earth. Apollo 11 prime crew was formally announced on Jan. 9, 1969, for a flight which was scheduled for July of that year. Armstrong, Collins and Aldrin all were experienced astronauts, each having flown one Gemini mission. Hardware for the Apollo 11 mission began arriving at the Kennedy Space Center (KSC) in January 1969 too, like the LM, the command/service module or the Saturn V rocket’s S-IVB third stage. Apollo11 The official NASA document dated June 26, 1969, and signed by Apollo Program Director Lt. Gen. Sam C. Phillips and Associate Administrator for Manned Flight George E. Mueller, worded the primary objective to Apollo 11 like 'perform a manned lunar landing and return.' In case Apollo 11 was not successful at accomplishing the first Moon landing in July 1969, NASA was prepared to try again with Apollo 12 in September, and if that proved unsuccessful as well, with Apollo 13 in December. On June 11, Apollo Program Director at NASA Headquarters announced that it was NASA's intention to carry out the first human lunar landing during the Apollo 11 mission in July pending successful completion of all required preflight activities. The decision was based on the results from the successful Apollo 10 mission and the readiness of mission preparations for Apollo 11. At the Kennedy Space Center (KSC), engineers completed the Flight Readiness Test (FRT) on June 6 and followed by early July by the Countdown Demonstration Test (CDDT). Because of the limited availability of the vehicle, only Apollo Commanders used the single-seat Lunar Landing Training Vehicle (LLTV). Lunar Module Pilots as well as Commanders used the Lunar Landing Research Facility (LLRF). In the Mission Control Center (MCC) three teams of flight controllers working eight-hour shifts monitored all aspects of the mission, led by experienced flight directors. The Green Team, led by Clifford E. Charlesworth, was the first shift, on console during the launch and the first few hours of the mission. The second shift, Eugene F. Kranz's White Team, was on console during the Moonlanding, while the Black Team led by Glynn S. Lunney comprised the third team. Flight Directors Milton L. Windler and Gerald D. Griffin provided assistance as required as a team of astronauts intimately familiar with all aspects of the mission served as Capsule Communicators, or Capcoms, talking directly with the crewmembers in space. Lunar Module Eagle landed in the Sea of Tranquility at 4:18 p.m. EDT on July, 20th. The stacking of the mission's elements occurred since April 1969 as April 14, Apollo Spacecraft Program Manager George M. Low announced in a press conference that Commander Neil A. Armstrong would most likely be the first person to exit the LM and take humanity's first steps on the lunar surface and that Lunar Module Pilot Edwin A. Buzz Aldrin would follow about 20 minutes later. The primary rationale for this decision was logistical -- because of the way the LM's hatch opened inward, it would be difficult at best for Aldrin to exit first, as he would need to climb over Armstrong in the cramped quarters of the cabin, both of them wearing bulky spacesuits. Future moonwalkers also trained for their mission during April. The Lunar Receiving Laboratory (LRL) fixed some troubles just prior mission's launch. Should anything have gone wrong during the first hours of the mission, Apollo 11 would have made an emergency splashdown in the Pacific Ocean about 1,600 miles southwest of Hawaii, where the USS Hornet carrier was ready since five hours before the Apollo 11 launch. Armstrong was first man to set foot on the Moon (same day, 10:56 p.m.). Neil Armstrong was likely chosen to be the first man on the Moon because he managed to regain control of the Gemini VIII capsule. "That's one small step for a man, one giant leap for mankind," he said when reaching the lunar soil. Surface exploration lasted 2½ h and 47 lbs of lunar material were collected. Apollo 11 science experiments to be deployed on the lunar surface were announced by November 1968, a passive seismometer, a laser ranging retro-reflector, and a solar wind composition experiment. The last only results would be brought home by mission's astronauts as both other could autonomously transmit or passively work. During their flight from Earth, the experiments were stowed in the Scientific Equipment Bay of the LM’s Descent Stage and crew manually retrieved the packages once on the lunar surface and deployed the experiments within 60 feet of the LM. It was NASA's DSS-1 antenna and tracking station which followed surface operations of Apollo 11. LM lift-off back to CSM occurred July 21st, 1969 1:54 p.m. EDT. Landing in Pacific Ocean was at 13° 30' N, 169° 15' E. When leaving the Moon's surface, the Apollo 11 crew were letting there the U.S. flag and a plaque, on the lower stage of the LM, bearing the inscription, 'Here men from the planet Earth first set foot upon the moon. July 1969 A.D. We came in peace for all mankind.' With his experience like a test pilot, Neil Armstrong was able to retake the control of the LEM from the autopilot and avoid a field of lunar rocks. That left the LEM with only 30 seconds of fuel at landing! Following their mission, the Apollo 11 three astonauts performed a world tour more on Apollo 11 | 8d 3h 18mn | ||
Apollo 12 | Nov 14th, 1969. Saturn V. 11:22 a.m. EST KSC (Complex 39-A) | Nov 24th, 1969 3:58 p.m. EST Pacific Ocean | Charles Conrad Jr (C), Richard Gordon Jr (CP), Alan Bean (LP) |
| 10d 4h 36mn | ||
Apollo 13 | April 11th, 1970. Saturn V. 2:13 p.m. EST KSC (Complex 39-A) | April 17th, 1970 1:07 p.m. EST Pacific Ocean | James Lovell Jr, John Swigert Jr, Fred Haise Jr | With NASA announcement in January 1970 of the cancellation of the final Moon landing mission, Apollo 20 schedule for the remaining Moon landing missions were stretched out, lengthening the interval between flights from four to six months. Mission target was Fra Mauro. In October 1969, Apollo 13 had been scheduled for a March 12, 1970, launch to visit the Fra Mauro highlands region of the Moon, with a geological emphasis. The Fra Mauro region was located about 110 miles east of the Apollo 12 touchdown point. Geologists favored the Fra Mauro area for exploration because it formed an extensive geologic unit around Mare Imbrium, the largest lava plain on the Moon. Unlike the Apollo 11 and 12 sites located in the flat lunar maria, Fra Mauro rested in the relatively more rugged lunar highlands. The precision landing by the Apollo 12 crew and their extensive orbital photography of the Fra Mauro region gave NASA confidence to attempt a landing at Fra Mauro. Two days before launch mission managers decided to replace prime Command Module Pilot (CMP) Thomas K. 'Ken' Mattingly with his backup John L. 'Jack' Swigert because Mattingly had been exposed to German measles or rubella, to which he had no natural immunity. Backup Lunar Module Pilot (LMP) Charles M. Duke contracted the rubella virus that causes German measles during a visit to friends and caught it from the son's three-year-old, thereby exposing the rest of the crew. Prime crew Commander James A. Lovell and LMP Fred W. Haise as well as backup Commander John W. Young and CMP Swigert all had natural immunity to the disease. Swigert completed several days of last minute refresher training and integrated well with Lovell and Haise as the new crew of Apollo 13. Mission was interrupted by a Service Module oxygen tank blow up (April 13th, 1970) as craft was heading Moon ("Hey Houston, we've had a problem here"). Crew had to find refuge in Lunar Module until return in Earth orbit. The mission eventually was classified as a 'successful failure' because of the experience gained in rescuing the crew. more on the Apollo 13 disaster | 5d 22h 54mn | ||
Apollo 14 | Jan 31st, 1971. Saturn V. 4:03 p.m. EST KSC (Complex 39) | Feb 9th, 1971 4:05 p.m. EST Pacific Ocean | Alan Shepard (C), Stuart Roosa (CP), Edgar Mitchell (LP) | As Fra Mauro (Apollo 13 mission) was of geological interest, Apollo 14 was directed to nearly the same place. As Apollo 14 original planned landing site at Littrow needed a training for a volcanic site, sending the crew at the Fra Mauro site needed subsequent training sessions. Apollo 14 also emphasized science observations from lunar orbit. That flight was a hard-fought return to flight for NASA's Apollo Program after the Apollo 13's failure. To honor the Wright brothers' accomplishment - - the U.S. inventors of flight - - Apollo 14 astronauts named their Lunar Module 'Kitty Hawk,' from the place in North Carolinia where they made their first flight. U.S. Air Force pilot Stuart Roosa and Naval aviator Edgar Mitchell were part of NASA's 5th group of astronauts. The descent to the Moon was plagued by two problems (a work-around reprogramming on the LM computer, or cycling the landing radar's breakers were needed). Surface operations astronauts traverse capability was improved due to the Modularized Equipment Transporter (a hand-drawn cart). During the mission, the commander's spacesuit was the first to use red stripes on the arms and legs and on the top of his helmet's sunshade, to better distinguish between him and LM pilot on the surface as identifier was used for the remaining Apollo missions, and the space shuttle missions further, and now on the ISS. Alan Shepard amusingly hit a golf ball on Moon. Docking the CSM to the Lunar Module required 6 tries over more than an hour and a half before the latches activated as a balky guidance system might have handicaped the landing. Crew, with two moon walks totaling 9h 21 mn, explorated a hilly zone about 300 miles from the edge of Mare Imbrium and the hills of Fra Mauro believed to be made of rubble blasted from the Imbrium impact. They failed however to reach the rim of Cone crater, a more recent impact crater about 1,000 feet wide a little over a mile from the lander, due to a hillier terrain. The crew deployed components of the Apollo Lunar Surface Experiments Package (ALSEP) on the surface. As Roosa had remain in orbit, he photographed the Moon, next landing sites included. Apollo 14 eventually splashed down approximately 760 miles South of American Samoa. The mission returned 100 pounds of rocks and soils and still holds the record for the longest walk on the moon, or approximately 9,000 feet. Pilot Roosa, on its personal allowance, carried and brought back varied tree seeds to the Moon as hundreds of 'moon trees' were distributed as seedlings | 9d 1mn 58s | ||
Apollo 15 | July 26th, 1971. Saturn V. 9:34 a.m. EDT KSC (Complex 39) | Aug 7th, 1971 4:45 p.m. EDT Pacific Ocean | David Scott (C), James Irwin (LP), Alfred Worden | Apollo 15 was the first of three science-oriented Apollo missions. Apollo 15 initiated missions endowed with Lunar Rover Vehicle (LRV). This Moon rover was able to reach a 10 mph speed extending exploration range. NASA's Marshall Space Flight Center designed, developed and managed the production of the Lunar Roving Vehicle. Surface operations took place in Hadley-Apennine region. Three moon walks totaled 18h 33 mn. Apollo 15 astronauts used the rover to make three separate trips beyond the Hadley-Apennine landing site. The rover endured a brief inoperability of the front steering mechanism as the crew proceeded on their initial traverse using only the rear-wheel steering. The LRV had been developed, designed and built by NASA's Marshall Space Flight Center. Lunar lift-off was TV broadcasted. Apollo mission planners selected an adventurous landing site for Apollo 15 located on a relatively small patch of a mare, a site nestled between the towering Apennine mountains to the East, and the valley of Hadley Rille to the West. The experience gained from the successful landings of the preceding Apollo missions afforded mission controllers confidence that a landing descending through a mountain range was possible. The LEM however ended with a tilted position at the surface. The Hadley Rille landing site also presented an opportunity to test the capabilities of the new lunar roving vehicle. Apollo 15's command module was the first to have its own module of scientific instruments. During the flight back from the Moon, one astronaut made three spacewalks to retrieve film from cameras in the module | 12d 7h 12mn | ||
Apollo 16 | April 16th, 1972. Saturn V. 12:54 p.m. EST KSC (Complex 39-A) | April 27th, 1972 2:45 p.m. EST Pacific Ocean | John Young (C), Thomas Mattingly II (CP), Charles Duke Jr (LP) | Target was Plain of Descartes as the Apollo 16 was the second of three science-oriented missions planned for the Apollo Program. Three moon walks totaled 20h 17mn. Crew stayed on Moon's surface about 71h as the mission also had been endwowed with a Lunar Roving Vehicle. A faulty CSM engine caused trouble about return Earth's route insertion but mission eventually succeeded. Apollo 16 astronauts were walking on the Moon in April 1972 when Mission Control informed them that the U.S. Congress had authorized the development of the Space Shuttle. Both astronauts enthusiastically responded to the positive news with 'Beautiful! Wonderful! Beautiful!' as astronaut Young added with some foresight, 'The country needs that shuttle mighty bad. You'll see.' Nine years later, he would be commanding the first ship of the space shuttle fleet, Columbia, on its maiden voyage. A telescope, called the 'Far Ultraviolet Camera/Spectrograph,' was used during the Apollo 16 mission checking celestial objects or the Earth's upper atmosphere. It remained on the Moon in the Descartes highland region | 11d 1h 51mn | ||
Apollo 17 | Dec 7th, 1972. Saturn V. 12:33 a.m. EST KSC (Complex 39) | Dec 19th, 1972 2:24 p.m. EST Pacific Ocean | Eugene Cernan (C), Ronald Evans, Harrison Schmitt (LP) | Last Apollo program mission. Three moon walks totaling 22h 2mn in a mare-rim highland contact region at Taurus-Littrow. The camera of the Lunar Rover Vehicle filmed the departure of the LM's ascent stage as Gene Cernan, commander of the mission, left the lunar surface with these words: "We leave as we came and, God willing, as we shall return, with peace, and hope for all mankind." | 12d 13h 52mn |