Apollo 13 was the seventh crewed mission in the Apollo space program and the third intended to land on the Moon. The craft was launched on April 11, 1970, from Kennedy Space Center, but the lunar landing was aborted after an oxygen tank in the service module (SM) exploded two days into the mission. The crew instead looped around the Moon, and returned safely to Earth on April 17, 1970, six days after launch. The mission was commanded by Jim Lovell with Jack Swigert as Command Module Pilot (CMP) and Fred Haise as Lunar Module Pilot (LMP). Swigert was a late replacement for the original CMP Ken Mattingly, who was grounded by the flight surgeon after exposure to German measles.
Apollo 13's damaged service module, photographed by the crew from the command module after jettisoning it shortly before reentry
|Mission type||Crewed lunar landing attempt|
|Mission duration||5 days, 22 hours, 54 minutes, 41 seconds|
|Launch mass||101,261 pounds (45,931 kg)|
|Landing mass||11,133 pounds (5,050 kg)|
|Start of mission|
|Launch date||April 11, 1970, 19:13:00UTC|
|Rocket||Saturn V SA-508|
|Launch site||Kennedy LC-39A|
|End of mission|
|Recovered by||USS Iwo Jima|
|Landing date||April 17, 1970, 18:07:41UTC|
|Landing site||South Pacific Ocean|
|Flyby of Moon (orbit and landing aborted)|
|Closest approach||April 15, 1970, 00:21:00 UTC|
|Distance||254 kilometers (137 nmi)|
|Docking with LM|
|Docking date||April 11, 1970, 22:32:08 UTC|
|Undocking date||April 17, 1970, 16:43:00 UTC|
Left to right Lovell, Swigert, Haise, 12 days after their return.
The explosion was caused by accidental ignition of damaged wire insulation inside an oxygen tank during a routine tank stirring operation. The accident resulted in a rapid loss of all oxygen in the service module, which was necessary for breathable air and for generating electrical power for the command module (CM). The command module's power had to be shut down to conserve its remaining resources for reentry, forcing the crew to transfer to the lunar module (LM) to power up its life support and navigational systems. These circumstances mandated an abort of the lunar landing and new procedures to bring the crew back to Earth alive.
Although the LM was designed to support two men on the lunar surface for two days, Mission Control in Houston drafted new procedures so it could support three men for four days. The crew experienced great hardship caused by limited power, loss of cabin heat, shortage of potable water, and the critical need to make makeshift repairs to the carbon dioxide removal system.
The flight passed the far side of the Moon at an altitude of 254 kilometers (137 nautical miles) above the lunar surface, and 400,171 km (248,655 mi) from Earth, a spaceflight record marking the farthest humans have traveled from Earth. The story of the Apollo 13 mission has been dramatized multiple times, most notably in the 1995 film Apollo 13.
Crew and key Mission Control personnel
Fourth and last spaceflight
|Command Module Pilot||Jack Swigert|
|Lunar Module Pilot||Fred Haise|
Lovell was born March 25, 1928 in Cleveland, Ohio. He initially attended the University of Wisconsin for two years but was appointed to the United States Naval Academy at Annapolis, Maryland, from which he graduated in 1952 with a Bachelor of Science degree. Becoming a naval aviator and test pilot, Lovell was selected as part of the second group of astronauts in 1962. A naval captain at the time of Apollo 13, he flew alongside Frank Borman in Gemini 7 and Buzz Aldrin in Gemini 12 before flying in Apollo 8 in 1968, the first spacecraft to orbit the Moon. Swigert was born on August 30, 1931 in Denver, Colorado. He earned a B.S. in mechanical engineering from the University of Colorado in 1953, later gaining a Master of Science degree in Aerospace Science from RPI in 1965, and in 1967 an MBA degree from the University of Hartford. He served in the Air Force and in state air national guards, and was an engineering test pilot prior to his selection as one of the fifth group of astronauts in 1966. Haise was born in Biloxi, Mississippi on November 14, 1933. He received a B.S. degree from the University of Oklahoma in 1959. He served in the Oklahoma Air National Guard and the United States Air Force, and was a civilian research pilot for NASA when he was selected alongside Swigert as a Group 5 astronaut.
According to the standard crew rotation in place during the Apollo program, the prime crew for Apollo 13 would have been the backup crew for Apollo 10 with Mercury and Gemini veteran Gordon Cooper in command, Donn F. Eisele as command module pilot (CMP) and Edgar Mitchell as lunar module pilot (LMP). Deke Slayton, NASA's Director of Flight Crew Operations, never intended to rotate Cooper and Eisele to another mission, as both were out of favor with NASA management for various reasons (Cooper for his lax attitude towards training, and Eisele for incidents aboard Apollo 7 and an extra-marital affair). He assigned them to the backup crew simply because of a lack of flight-qualified manpower in the Astronaut Office at the time the assignment needed to be made. Slayton felt Cooper had no more than a very small chance of receiving the Apollo 13 command, if he did an outstanding job with the assignment, which he did not. Slayton always intended to assign Eisele to a future Apollo Applications Program mission rather than a lunar mission, but this program was eventually cut down to only the Skylab component.
Thus, the original assignment Slayton submitted to his superiors for this flight was Commander Alan Shepard, Command Module Pilot Stuart Roosa and Lunar Module Pilot Edgar Mitchell. For the first time ever, Slayton's recommendation was rejected by management, who felt that Shepard needed more time to train properly for a lunar flight, as he had only resumed active astronaut status after undergoing experimental surgery to correct an inner ear disorder which had kept him grounded since his Mercury flight in 1961. Thus, Lovell's crew, backup for the historic Apollo 11 mission and therefore slated for Apollo 14, was swapped with Shepard's making the prime crew for Apollo 13:
|Command Module Pilot||Ken Mattingly|
|Lunar Module Pilot||Fred Haise|
NASA assigned a backup crew of John Young as commander, Jack Swigert as command module pilot and Charles Duke as lunar module pilot. Seven days before launch, Duke contracted rubella from one of his children. This exposed both the prime and backup crews, who trained together. Mattingly was found to be the only one of the other five who had not had rubella as a child and thus was not immune. Three days before launch, at the insistence of the Flight Surgeon, Swigert was moved to the prime crew.
Mattingly never contracted rubella and was assigned after the mission as command module pilot for Young's crew, which flew Apollo 16, the fifth mission to land on the Moon.
- Gene Kranz – White team; (lead)
- Glynn Lunney – Black team;
- Milt Windler – Maroon team;
- Gerry Griffin – Gold team.
The CAPCOMs were Kerwin, Brand, Lousma, Young and Mattingly.
Mission insignia and call signs
The Apollo 13 mission insignia depicts the Greek god of the Sun, Apollo, with three horses pulling his chariot across the face of the Moon, and the Earth seen in the distance. This is meant to symbolize the Apollo flights bringing the light of knowledge to all people. The motto, Ex luna, scientia means "From the Moon, knowledge".
The mission insignia was sculpted as a medallion, Steeds of Apollo by Lumen Martin Winter. and was painted as a mural on the wall of a Chicago-area restaurant owned by one of Lovell's children. That representation shows four horses, one for each member of the crew who flew, and the fourth for Mattingly.
The motto was in Lovell's mind when he chose the call sign Aquarius for the lunar module, taken from Aquarius, the bringer of water. Some from the media erroneously reported that the call sign was taken from a song by that name from the musical Hair. The command module's call sign, Odyssey, was chosen not only for its Homeric association but to refer to the recent movie, 2001: A Space Odyssey, based on a short story by science fiction author Arthur C. Clarke. In his book, Lovell indicated he chose the name Odyssey because he simply liked the word and its definition: a long voyage with many changes of fortune.
Hardware and mission preparation
Launch vehicle and spacecraft
The Saturn V used to carry Apollo 13 to the Moon was numbered SA-508, and was almost identical to those used on Apollo 8 through 12. Including the spacecraft, the rocket was 25,600 pounds (11,600 kg) heavier than Apollo 12's. The S1-C engines were rated at 100,000 pounds (45,000 kg) less total thrust than Apollo 12's, though they remained within specifications. Extra fuel was carried; the reason for this was in part as a preliminary to the future J missions to the Moon that would carry heavier payloads. This made the vehicle the heaviest yet flown by NASA and made Apollo 13 visibly slower to clear the launch tower than earlier missions.
On previous missions, the S-IVB third stage had been sent into solar orbit once the spacecraft detached from it. At the First Lunar Science Conference in January 1970, it was revealed that while the seismometer left by Apollo 12 had detected almost daily impacts of objects onto the Moon, none had been as large as that of Apollo 12's LM, Intrepid, which had been deorbited after being jettisoned. In the hope larger impacts would allow scientists on Earth to probe the structure of the Moon's crust, it was decided that beginning with Apollo 13, the launch vehicle's S-IVB stage would be crashed into the Moon.
The Apollo 13 spacecraft consisted of Command Module 109 and Service Module 109 (together CSM-109), called Odyssey, and Lunar Module 7 (LM–7), called Aquarius. Also considered part of the spacecraft were the Launch Escape System which would propel the CM to safety in the event of a problem during launch, and the Spacecraft–LM Adapter, numbered as SLA–16, which housed the LM during the first hours of the mission.
Concerned about how close Apollo 11's LM, Eagle, had come to running out of fuel during its lunar descent, mission planners decided that beginning with Apollo 13, the CSM would bring the LM to the low orbit from which the landing attempt would commence. This was a change from Apollo 11 and 12, on which the LM made the burn to bring it to the lower orbit. The change was part of an effort to increase the amount of hover time available to the astronauts as the missions headed into rougher terrain.
ALSEP and other equipment
Apollo 11 had left a seismometer on the Moon, but the solar-powered unit did not survive its first two-week-long lunar night. The Apollo 12 astronauts also left one as part of its ALSEP installation of nuclear-powered scientific instruments. Apollo 13 carried a seismometer similar to Apollo 12's as part of its ALSEP package, which was carried in the LM descent stage's scientific equipment bay. That seismometer was to be calibrated by the impact, after jettison, of the ascent stage of Apollo 13's LM, an object of known mass and velocity impacting at a known location.
Other ALSEP experiments included a Heat Flow Experiment, which would involve the drilling of two holes 10 feet (3.0 m) deep. This was Haise's responsibility; he was also to drill a third hole of that depth for a core sample. A Charged Particle Lunar Environment Experiment (CPLEE) measured the protons and electrons of solar origin reaching the Moon. The package also included a Lunar Atmosphere Detector and a Dust Detector, to measure the accumulation of debris on the ALSEP. The heat flow experiment and the CPLEE were flown for the first time on Apollo 13; the other experiments had been flown before.
To power the ALSEP, the SNAP-27 radioisotope thermoelectric generator was flown. Developed by the U.S. Atomic Energy Commission, SNAP-27 was first flown on Apollo 12. The fuel capsule contained about 8.36 pounds (3.79 kg) of plutonium oxide. The cask placed around the capsule for transport to the Moon was built with heat shields of graphite and of beryllium, with structural parts of titanium and of Inconel materials. Thus, it was built to take the heat of re-entry into the Earth's atmosphere without coming apart, as the Apollo 13 Press Kit put it, "in the unlikely event of an aborted mission".
Like Apollo 11 and 12, Apollo 13 flew the Solar Wind Composition Experiment, a windowshade-like device that would be deployed on the lunar surface and then be folded up and brought back by the astronauts. It also flew the Lunar Stereo Closeup Camera, intended to show the fine structure of lunar rocks and soil. A United States flag was also taken, to be erected on the Moon's surface. For Apollo 11 and 12, the flag had been placed in a heat-resistant tube on the front landing leg; it was moved for Apollo 13 to the Modularized Equipment Stowage Assembly (MESA) in the LM descent stage. The structure to fly the flag on the airless Moon was improved from Apollo 12's.
For the first time, red stripes were placed on the helmet, arms and legs of the commander's A7L spacesuit. This was done as after Apollo 11, those reviewing the images taken had trouble distinguishing Armstrong from Aldrin, but the change was approved too late for Apollo 12. The Apollo 12 moon walkers had gotten thirsty during their lunar surface activities; the new drink bags that could be placed inside the helmets and sipped from as the astronauts explored were demonstrated by Haise during Apollo 13's final television broadcast before the accident.
Landing site selection; astronaut training
Apollo 12 had shown that lunar astronauts could perform a precision landing. Thus, mission planners for Apollo 13 were able to seek a smaller landing target someplace other than the lunar mares, or seas, upon which Apollo 11 and 12 had set down. Apollo 11 and 12 each had a backup site for landing in case of launch delays; this requirement also was deleted for Apollo 13. This did not open up the whole Moon to planners—sites still had to be in the equatorial region of the near side —but they could be more flexible and could seek a site of greater scientific interest.
In anticipation of successful lunar landings, the Site Selection Board met in June 1969 to plan Apollo 13, and a site near Fra Mauro crater gained consensus. The Fra Mauro formation was believed to contain much material spattered by the impact that had filled the Imbrium basin, early in the Moon's history. Dating it would provide information not only about the Moon, but about the Earth's early history. The landing site was about 26 miles (42 km) north of Fra Mauro crater itself, near what was dubbed Cone crater, a site where an impact was believed to have drilled deep into the lunar regolith. Due to the roughness of the terrain, the selected landing site was over a mile (two kilometers) from Cone crater, but Lovell, who as commander was to perform the landing, had the option of setting down closer if he believed he could do so safely. NASA initially had few high-quality photographs of that location, but after Dick Gordon, CMP of Apollo 12, took more from orbit in November 1969, Fra Mauro was confirmed as Apollo 13's landing site.
A month before the planned landing, Lovell and Haise undertook a mock EVA at Arizona's Verde Valley, over a landscape made to look as much like the lunar surface as possible. The Apollo 13 prime crew undertook over 1,000 hours of mission-specific training, more than five hours for every hour of the mission's ten-day planned duration. Each member of the prime crew spent over 400 hours in simulators of the CM and of the LM at Kennedy Space Center (KSC) and at Houston, some of which involved the flight controllers at Mission Control. Specialized simulators at other locations were also used.
The plan was to devote the first of the two four-hour lunar surface EVAs to setting up the ALSEP; during the second, Aquarius's crew would investigate Cone crater. Lovell and Haise wore their spacesuits for some 20 walk-throughs of EVA procedures, including sample gathering and use of tools and other equipment. The astronauts flew in the "Vomit Comet" in simulated microgravity or lunar gravity, including practice in donning and doffing spacesuits. To prepare for the descent to the Moon's surface, Lovell flew the Lunar Landing Training Vehicle (LLTV). Despite the fact that four of the five LLTVs and similar Lunar Landing Research Vehicles crashed during the course of the Apollo program, mission commanders considered flying them invaluable experience.
Preparation and objectives
The LM stages, CM and SM were received at KSC in June 1969; the portions of the Saturn V were received in June and July. Thereafter, testing and assembly proceeded, culminating with the rollout of the launch vehicle, with the spacecraft atop it, on December 15, 1969. Apollo 13 was originally scheduled for launch on March 12, 1970; in January of that year NASA announced the mission would be postponed until April 11, both to allow additional time for planning and to spread out the Apollo missions over a longer period of time.
In addition to the goals associated with the lunar landing, the astronauts of Apollo 13 were to accomplish a number of photographic objectives: of candidate sites for future Moon landings, of the Gegenschein from lunar orbit, and of the Moon itself on the journey back to Earth. Some of this photography was to be performed by Swigert as Lovell and Haise walked on the Moon. The command module pilot was also to take photographs of the Lagrangian points of the Earth-Moon system. Apollo 13 had twelve cameras onboard, including those for television and moving pictures. The crew was also to downlink bistatic radar observations of the Moon. None of these goals could be attempted because of the accident that damaged the spacecraft.
Several of the experiments for Apollo 13 were completed despite the aborted mission. An experiment to measure the amount of atmospheric electrical phenomena during the ascent to orbit had been added after Apollo 12 was struck by lightning; it returned data indicating a heightened risk during marginal weather. A series of photographs of Earth was taken to test whether a determination of cloud height could be made from synchronous satellites; this achieved the desired results. The third successful experiment, Seismic Detection of Third-Stage Lunar Impact, was the Apollo 12 seismometer's detection of the S-IVB's impact when it hit the Moon.
Flight of Apollo 13
Launch and translunar injection
The mission was launched at the planned time, 02:13:00 PM EST (19:13:00 UTC) on April 11. An anomaly occurred when the second-stage, center (inboard) engine shut down about two minutes early. The four outboard engines and the third-stage engine burned longer to compensate, and the vehicle achieved very close to the planned circular 100 nautical miles (190 km) parking orbit, followed by a normal translunar injection about two hours later. The engine shutdown was determined to be caused by severe pogo oscillations measured at a strength of 68 g and a frequency of 16 hertz, causing the thrust frame to flex by 3 inches (76 mm). The vehicle's guidance system shut the engine down in response to sensed thrust chamber pressure fluctuations. Pogo oscillations had been seen on previous Titan rockets, and also on the Saturn V during the uncrewed Apollo 6 mission, but on Apollo 13, they were amplified by an unexpected interaction with turbopump cavitation, caused by pressure that was low, but within specifications, inside the S-II's liquid oxygen system. Fixes were already under development by NASA, but time did not permit their inclusion for Apollo 13.
Swigert performed the separation and transposition maneuvers before docking the CSM Odyssey to the LM Aquarius, and the spacecraft pulled away from the third stage, which ground controllers then sent on a course to impact the Moon in range of the Apollo 12 seismometer. The impact occurred at 77:56:40 into the mission, about 22 hours after the accident, and produced such strong signals in the Moon that the gain on that seismometer, 73 miles (117 km) from the impact, had to be turned down.
The crew settled in for the three-day trip to Fra Mauro. At 30:40:50 into the mission, with the TV camera running, the crew performed a burn to place Apollo 13 on a hybrid trajectory. This was necessary to reach Fra Mauro, but the departure from a free return trajectory meant that if no further burns were performed, Apollo 13 would miss Earth by some 40,000 miles (64,000 km), rather than intercept it, as with a free return.
Accident: "Houston, we've had a problem"
Approaching 56 hours into the mission, Apollo 13 was approximately 205,000 miles (330,000 km) from Earth en route to the Moon. Approximately six and a half minutes after the end of a live TV broadcast from the spacecraft, Haise was in the process of closing out the LM, while Lovell was stowing the TV camera. Houston flight controllers asked Swigert to turn on the hydrogen and oxygen tank stirring fans in the service module, which were designed to destratify the cryogenic contents and increase the accuracy of their quantity readings. Two minutes later, the astronauts heard a "pretty large bang," accompanied by fluctuations in electrical power and the firing of the attitude control thrusters; the crew initially thought that a meteoroid might have struck the lunar module. Communications and telemetry to Earth were lost for 1.8 seconds, until the system automatically corrected by switching the high-gain S-band antenna, used for translunar communications, from narrow-beam to wide-beam mode.
Immediately after the bang, Swigert reported "Okay, Houston, we've had a problem here," which Lovell repeated and clarified as a "main B bus undervolt," a temporary loss of operating voltage on the second of the spacecraft's main electrical circuits. Oxygen tank 2 immediately read quantity zero. About three minutes later, the number 1 and number 3 fuel cells failed. Lovell reported seeing out the window that the craft was venting "a gas of some sort" into space. The number 1 oxygen tank quantity gradually reduced to zero over the next 130 minutes, entirely depleting the SM's oxygen supply.
Because the fuel cells generated the command and service module's electrical power by combining hydrogen and oxygen into water, when oxygen tank 1 ran dry, the remaining fuel cell finally shut down, leaving the craft on the command module's limited-duration battery power and water. The crew was forced to shut down the CM completely to save this for reentry, and to power up the LM to use as a "lifeboat." This situation had been suggested during an earlier training simulation, but had not been considered a likely scenario. Without the LM, the accident would certainly have been fatal.
Crew survival and return journey
The damage to the service module made safe return from a lunar landing impossible, so Lead Flight Director Gene Kranz ordered an abort of the mission. The existing abort plans, first drawn up in 1966, were evaluated; the quickest was a Direct Abort trajectory, which required using the service propulsion system (SPS) engine to achieve a 6,079-foot-per-second (1,853 m/s) delta-v.p. III-14 Although a successful SPS firing at 60 hours ground elapsed time (GET) would land the crew one day earlier (at 118 hours GET, or 58 hours later), the large delta-v was possible only if the LM were jettisoned first,p. II-1 and since crew survival depended on the LM's presence during the coast back to Earth, that option was "out of the question."p. III-17 An alternative would have been to burn the SPS fuel to depletion, then jettison the service module and make a second burn with the LM Descent Propulsion System (DPS) engine. It was desired to keep the service module attached for as long as possible because of the thermal protection it afforded the command module's heat shield. Apollo 13 was close to entering the lunar sphere of gravitational influence (at 61 hours GET), which was the break-even point between direct and circumlunar aborts, and the latter allowed more time for evaluation and planning before a major rocket burn.p. B-5 There also was concern about "the structural integrity of the Service Module,"p. III‑23 so mission planners were instructed that the SPS engine would not be used "except as a last-ditch effort."p. III-14
For these reasons, Kranz chose the alternative circumlunar option, using the Moon's gravity to return the ship to Earth. Apollo 13 had left its initial free-return trajectory earlier in the mission, as required for the lunar landing at Fra Mauro. Therefore, the first order of business was to re-establish the free-return trajectory with a 30.7-second burn of the DPS. The descent engine was used again two hours after pericynthion, the closest approach to the Moon ("PC+2 burn"), to speed the return to Earth by 10 hours and move the landing spot from the Indian Ocean to the Pacific Ocean. A more aggressive burn could have been performed at PC+2 by first jettisoning the service module, returning the crew in about the same amount of time as a direct abort,p. III-20 but this was deemed unnecessary given the rates at which consumables were being used. The 4-minute, 24-second burn was so accurate that only two more small course corrections were subsequently needed.
Considerable ingenuity under extreme pressure was required from the crew, flight controllers, and support personnel for the safe return. The developing drama was shown on television. Because electrical power was severely limited, no more live TV broadcasts were made; TV commentators used models and animated footage as illustrations. Low power levels made even voice communications difficult.
The lunar module consumables were intended to sustain two people for a day and a half, not three people for four days. Oxygen was the least critical consumable because the LM carried enough to repressurize the LM after each surface EVA. Unlike the command and service module (CSM), which was powered by fuel cells that produced water as a byproduct, the LM was powered by silver-zinc batteries, so electrical power and water (used for equipment cooling as well as drinking) were critical consumables. To keep the LM life-support and communication systems operational until reentry, the LM was powered down to the lowest levels possible. In particular, the LM's Abort Guidance System was used for most of the coast back to Earth instead of the primary guidance system, as it used less power and water.pp. III‑17,33,40
Availability of lithium hydroxide (LiOH) for removing carbon dioxide presented a serious problem. The LM's internal stock of LiOH canisters was not sufficient to support the crew until return, and the remainder was stored in the descent stage, out of reach. The CM had an adequate supply of canisters, but these were incompatible with the LM. Engineers on the ground improvised a way to join the cube-shaped CM canisters to the LM's cylindrical canister-sockets by drawing air through them with a suit return hose. NASA engineers referred to the improvised device as "the mailbox."
Another problem to be solved for a safe return was accomplishing a complete power-up from scratch of the completely shut-down command module, something never intended to be done in-flight. Flight controller John Aaron, with the support of grounded astronaut Mattingly and many engineers and designers, had to invent a new procedure to do this with the ship's limited power supply and time factor. This was further complicated by the fact that the reduced power levels in the LM caused internal temperatures to drop to as low as 4 °C (39 °F). The unpowered CM got so cold that water began to condense on solid surfaces, causing concern that this might short out electrical systems when it was reactivated. This turned out not to be a problem, partly because of the extensive electrical insulation improvements instituted after the Apollo 1 fire.
The last problem to be solved was how to separate the lunar module a safe distance away from the command module just before reentry. The normal procedure was to use the service module's reaction control system (RCS) to pull the CSM away after releasing the LM along with the command module's docking ring, but this RCS was inoperative because of the power failure, and the useless SM would be released before the LM. Grumman called a team of six University of Toronto engineers, led by senior scientist Bernard Etkin, to solve the problem within a day. The team concluded that pressurizing the tunnel connecting the lunar module to the command module just before separation would provide the force necessary to push the two modules a safe distance away from each other just prior to reentry. The team had 6 hours to accurately compute the pressure required, using slide rules. Too high a pressure could damage the hatch and its seal, endangering the astronauts on reentry; too low and the lunar module would not be sufficiently separated. Grumman relayed their calculation to NASA, and from there in turn to the astronauts, who used it successfully.
Reentry and splashdown
As Apollo 13 neared Earth, the crew first jettisoned the service module, using the LM's reaction control system to pull themselves a safe distance from it, instead of the normal procedure which used automatic firing of the SM's RCS. They photographed it for later analysis of the accident's cause. It was then that the crew were surprised to see for the first time that the entire Sector 4 panel had been blown off. According to the analysts, these pictures also showed the antenna damage and possibly an upward tilt to the fuel cell shelf above the oxygen tank compartment.
The command module Odyssey was the only part of the spacecraft capable of reentry through the atmosphere. All three crew were therefore inside it when they jettisoned the lunar module Aquarius using the above procedure worked out at the University of Toronto, in final preparation for reentry.
The reentry on a lunar mission was typically accompanied by about four minutes of communications blackout caused by ionization of the air around the command module. The blackout in Apollo 13's reentry lasted six minutes, which was 87 seconds longer than had been expected. The possibility of heat-shield damage from the O
2 tank rupture heightened the tension of the blackout period.
Odyssey regained radio contact and splashed down safely in the South Pacific Ocean, American Samoa and 6.5 km (3.5 nmi) from the recovery ship, USS Iwo Jima. The crew was in good condition except for Haise, who was suffering from a serious urinary tract infection because of insufficient water intake. To avoid altering the trajectory of the spacecraft, the crew had been instructed to temporarily stop urine dumps, which forced them to invent ways of storing all urine for the rest of the flight., southeast of
The lunar module and service module reentered the atmosphere over the South Pacific between the islands of Fiji and New Zealand.
The crew on board the USS Iwo Jima following splashdown
Public and media reaction
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Investigation and response
NASA Administrator Thomas Paine and Deputy Administrator George Low sent a memorandum to NASA Langley Research Center Director Edgar M. Cortright on April 17, 1970, (date of spacecraft splashdown) advising him of his appointment as chairman of an Apollo 13 Review Board to investigate the cause of the accident.
The second memorandum to Cortright from Paine and Low on April 21 established the board as follows:
- Robert F. Allnutt (Assistant to the Administrator, NASA Hqs.);
- Neil Armstrong (Astronaut, Manned Spacecraft Center);
- Dr. John F. Clark (Director, Goddard Space Flight Center);
- Brig. General Walter R. Hedrick Jr. (Director of Space, DCS/RED, Hqs., USAF);
- Vincent L. Johnson (Deputy Associate Administrator-Engineering, Office of Space Science and Applications);
- Milton Klein (Manager, AEC-NASA Space Nuclear Propulsion Office);
- Dr. Hans M. Mark (Director, Ames Research Center).
- George Malley (Chief Counsel, Langley Research Center)
- Charles W. Mathews (Deputy Associate Administrator, Office of Manned Space Flight)
- William A. Anders (Executive Secretary, National Aeronautics and Space Council; ex-astronaut);
- Dr. Charles D. Harrington (Chairman, NASA Aerospace Safety Advisory Panel);
- I. I. Pinkel (Director, Aerospace Safety Research and Data Institute, Lewis Research Center).
- Gerald J. Mossinghoff (Office of Legislative Affairs, NASA Hqs.)
- Brian Duff (Public Affairs Officer. Manned Spacecraft Center)
Activities and report
The board exhaustively investigated and analyzed the history of the manufacture and testing of the oxygen tank, and its installation and testing in the spacecraft up to the Apollo 13 launch, as documented in detailed records and logs. They visited and consulted with engineers at the contractor's sites and the Kennedy Space Center. Once a theory of the cause was developed, elements of it were tested, including on a test rig simulation in a vacuum chamber, with a damaged tank installed in the fuel cell bay. This test confirmed the theory when a similar explosion was created, which blew off the outer panel exactly as happened in the flight. Cortright sent the final Report of Apollo 13 Review Board to Administrator Paine on June 15, 1970.
The failure started in the service module's number 2 oxygen tank. Damaged Teflon insulation on the wires to the stirring fan inside oxygen tank 2 allowed the wires to short-circuit and ignite this insulation. The resulting fire rapidly increased pressure beyond its 1,000-pound-per-square-inch (6.9 MPa) limit and the tank dome failed, filling the fuel cell bay (Sector 4) with rapidly expanding gaseous oxygen and combustion products. It is also possible some combustion occurred of the Mylar/Kapton thermal insulation material used to line the oxygen shelf compartment in this bay.
The resulting pressure inside the compartment popped the bolts attaching the 13-foot (4.0 m) Sector 4 outer aluminum skin panel, which as it blew off probably caused minor damage to the nearby S-band antenna.
Mechanical shock forced the oxygen valves closed on the number 1 and number 3 fuel cells, leaving them operating for only about three minutes on the oxygen in the feed lines. The shock also either partially ruptured a line from the number 1 oxygen tank, or caused its check or relief valve to leak, causing its contents to leak out into space over the next 130 minutes, entirely depleting the SM's oxygen supply.
The board determined the oxygen tank failure was caused by an unlikely chain of events. Tanks storing cryogens, such as liquid oxygen and liquid hydrogen, require either venting, extremely good insulation, or both, in order to avoid excessive pressure buildup due to vaporization of the tanks' contents. The service module oxygen tanks were so well insulated that they could safely contain supercritical hydrogen and oxygen for years. Each oxygen tank held several hundred pounds of oxygen, which was used for breathable air and the production of electricity and water. The construction of the tanks made internal inspection impossible.
The tank contained several components relevant to the accident:
- a quantity sensor;
- a fan to stir the tank contents for more accurate quantity measurements;
- a heater to vaporize liquid oxygen as needed;
- a thermostat to protect the heater;
- a temperature sensor;
- fill and drain valves and piping.
The heater and protection thermostats were originally designed for the command module's 28-volt DC bus. The specifications for the heater and thermostat were later changed to allow a 65-volt ground supply, in order to pressurize the tanks more rapidly. Beechcraft, the tank subcontractor, did not upgrade the thermostat to handle the higher voltage.
The oxygen shelf carrying the oxygen tanks was originally installed in the Apollo 10 service module, but was removed to fix a potential electromagnetic interference problem. During removal, the shelf was accidentally dropped about 2 inches (5 cm) because a retaining bolt had not been removed. The tank appeared to be undamaged, but a loosely fitting filling tube was apparently damaged, and photographs suggested that the close-out cap on the top of the tank may have hit the fuel cell shelf. The report of the Apollo 13 review board considers the probability of tank damage during this incident to be "rather low". After the tank was filled for ground testing, it could not be emptied through the normal drain line. To avoid delaying the mission by replacing the tank, the heater was connected to 65-volt ground power to boil off the oxygen. Lovell signed off on this procedure. It should have taken a few days at the thermostatic opening temperature of 27 °C (81 °F). When the thermostat opened, the 65-volt supply fused its contacts closed and the heater remained powered. The board confirmed by testing that the thermostats welded themselves closed under the higher voltage. This raised the temperature of the heater to an estimated 540 °C (1,000 °F). A chart recorder on the heater current showed that the heater was not cycling on and off, as it should have been if the thermostat was functioning correctly, but no one noticed it at the time. Because the temperature sensor was not designed to read higher than the 27 °C (81 °F) thermostat opening temperature, the monitoring equipment did not register the true temperature inside the tank. The gas boiled off in hours rather than days.
The sustained high temperatures melted the Teflon insulation on the fan power supply wires and left them exposed. When the tank was refilled with oxygen, it became a bomb waiting to go off. During the "cryo stir" procedure, fan power passed through the bare wires which apparently shorted, producing sparks and igniting the Teflon. This in turn boiled liquid oxygen faster than the tank vent could remove it.
In June 1970, the Cortright Report provided an in-depth analysis of the mission in an extremely detailed five-chapter report with eight appendices. It included a copy of established NASA procedures for alleviating high pressure in a cryogenic oxygen tank, to include:
- Turning the four tank heaters and fans off;
- Pulling the two heater circuit breakers to open to remove the energy source;
- Performing a 2-minute purge, or directly opening the O2 valve.
This procedure was designed to prevent hardware failure so that the lunar landing mission could be continued. The Mission Operations Report Apollo 13 recounts how the master caution and warning alarm had been turned off for a previous low-pressure reading on hydrogen tank 2, and so it did not trigger to call attention to the high oxygen pressure reading.
Oxygen tank 2 was not the only pressure vessel that failed during this mission. Prior to the accident, the crew had moved the scheduled entry into the lunar module forward by three hours. This was done to get an earlier look at the pressure reading of the supercritical helium (SHe) tank in the LM descent stage, which had been suspect since before launch. After the abort decision, the helium pressure continued to rise and Mission Control predicted the time that the burst disc would rupture. The helium tank burst disc ruptured at 108:54, after the lunar flyby. The expulsion reversed the direction of the passive thermal control (PTC) roll (nicknamed the "barbecue roll").
While the investigation board did recreate the oxygen tank failure, it did not report on any experiments that would show how effective the Cryogenic Malfunctions Procedures were to prevent the system failure by de-energizing the electrical heater and fan circuits.
The oxygen tank was redesigned, with the thermostats upgraded to handle the proper voltage. The heaters were retained since they were necessary to maintain oxygen pressure. The stirring fans, with their unsealed motors, were removed, which meant the oxygen quantity gauge was no longer accurate. This required adding a third tank so that no tank would go below half full.
All electrical wiring in the power system bay was sheathed in stainless steel, and the oxygen quantity probes were changed from aluminum to stainless steel. The fuel cell oxygen supply valves were redesigned to isolate the Teflon-coated wiring from the oxygen. The spacecraft and Mission Control monitoring systems were modified to give more immediate and visible warnings of anomalies.
Because Apollo 13 followed the free-return trajectory, its altitude over the lunar far side was approximately 100 km (60 mi) greater than the orbital altitude on the remaining Apollo lunar missions. The Moon was almost at apogee during the mission (as it also was during the flights of Apollo 10 and Apollo 15), which also increased the distance from the Earth. The combination of the two effects ensures that Apollo 13 holds the absolute altitude record for a crewed spacecraft, reaching a distance of 400,171 kilometers (248,655 mi) from Earth on 7:21 pm EST, April 14, 1970.
The Apollo 13 mission was called a "successful failure" by Lovell, because of the successful safe return of the astronauts, but the failed lunar landing. It has also been termed "NASA's finest hour".
President Nixon flew to Houston to award the Apollo 13 Mission Operations Team the Presidential Medal of Freedom on April 18. Because the Medal of Freedom was presented as a group award, the members of the Apollo 13 team have the distinction of being the only individuals ever presented with the honor without being given the actual medal itself. He then flew to Honolulu to award the crew the Presidential Medal of Freedom for their actions during the mission.
The Cold Cathode Gauge Experiment (CCGE) which was part of the ALSEP on Apollo 13 was never flown again. It was a version of the Cold Cathode Ion Gauge (CCIG) which featured on Apollo 12, Apollo 14, and Apollo 15. The CCGE was designed as a standalone version of the CCIG. On other missions, the CCIG was connected as part of the Suprathermal Ion Detector (SIDE). Because of the aborted landing, this experiment was never deployed. Other experiments included on Apollo 13's ALSEP included the Heat Flow Experiment (HFE), the Passive Seismic Experiment (PSE), and the Charged Particle Lunar Environment Experiment (CPLEE).
Plaque and insignia
The original lunar plaque affixed to the front landing leg of Aquarius bore Mattingly's name, so a replacement plaque with Swigert's name was carried in the cabin, for Lovell to place over the other after he descended the ladder. He kept the plaque as a souvenir. In his book Lost Moon (later renamed Apollo 13), Lovell stated that, apart from the plaque and a couple of other pieces, the only other memento he possesses is a letter from Charles Lindbergh.
The Apollo 13 crew patch featured three flying horses as Apollo's "chariot" across space. Given Lovell's Navy background, the logo also included the mottoes "Ex Luna, scientia" ("From the Moon, knowledge"), borrowed from the U.S. Naval Academy's motto, "Ex scientia tridens" ("From knowledge, sea power"). The mission number appeared in Roman numerals as Apollo XIII. The patch did not have to be modified after Mattingly's replacement since it is one of only two Apollo mission insignia—the other being Apollo 11—not to include the names of the crew. It was designed by artist Lumen Martin Winter, who based it on a mural he had done for The St. Regis Hotel in New York City. The mural was later purchased by actor Tom Hanks, who portrayed Lovell in the movie Apollo 13, and now is on the wall of a restaurant near Chicago owned by Lovell's son.
Despite Apollo 13's failure to land on the Moon, several experiments were conducted successfully because they were initiated before or conducted independently of the oxygen tank explosion.
- Several experiments to study electrical phenomena were conducted prior to and during the launch of Apollo 13. This information was used to better understand hazards of launching in less than ideal weather conditions.
- Eleven photographs of Earth were taken at precisely recorded times, to study the feasibility of using geosynchronous satellites to study cloud height.
- Apollo 13's S-IVB third stage was the first to be purposely crashed into the lunar surface, as an active seismic experiment which measured its impact with a seismometer left on the lunar surface by the crew of Apollo 12. (The S-IVBs from the previous four lunar missions were sent into solar orbit by ground control after use.)
As a joke following Apollo 13's successful splashdown, Grumman Aerospace Corporation pilot Sam Greenberg (who had helped with the strategy for re-routing power from the LM to the crippled CM) issued a tongue-in-cheek invoice for $400,540.05 to North American Rockwell, Pratt and Whitney, and Beech Aircraft, prime and subcontractors for the CSM, for "towing" the crippled ship most of the way to the Moon and back. The figure was based on an estimated 400,001 miles (643,739 km) at $1.00 per mile, plus $4.00 for the first mile. An extra $536.05 was included for battery charging, oxygen, and an "additional guest in room" (Swigert). A 20% "commercial discount," as well as a further 2% discount if North American were to pay in cash, reduced the total to $312,421.24. North American declined payment, noting that it had ferried three previous Grumman LMs to the Moon (Apollo 10, Apollo 11 and Apollo 12) with no such reciprocal charges.
The command module shell was formerly at the Musée de l'air et de l'espace, in Paris. The interior components were removed during the investigation of the accident and reassembled into boilerplate BP-1102A, the water egress training module; and were subsequently on display at the Museum of Natural History and Science in Louisville, Kentucky, until 2000. The command module and the internal components were reassembled, and Odyssey is currently on display at the Cosmosphere in Hutchinson, Kansas.
The lunar module burned up in Earth's atmosphere on April 17, 1970, having been targeted to enter over the Pacific Ocean to reduce the possibility of contamination from a SNAP 27 radioisotope thermoelectric generator (RTG) on board. Intended to power the mission's ALSEP, the RTG survived reentry (as designed) and landed in the Tonga Trench. While it will remain radioactive for several thousand years, it does not appear to be releasing any of its 3.9 kg of radioactive plutonium-238.
Popular culture and media
The 1974 movie Houston, We've Got a Problem, while set around the Apollo 13 incident, is a fictional drama about the crises faced by ground personnel when the emergency disrupts their work schedules and places additional stress on their lives; only a couple of news clips and a narrator's solemn voice deal with the actual problems. "Houston ... We've Got a Problem" was also the title of an episode of the BBC documentary series A Life At Stake, broadcast in March 1978. This was an accurate, if simplified, reconstruction of the events.
Lovell was approached in 1991 by journalist Jeffrey Kluger about collaborating on a non-fiction account of the mission. The resultant book, Lost Moon: The Perilous Voyage of Apollo 13, was published in 1994.
The next year, in 1995, a film adaptation of the book, Apollo 13, was released, directed by Ron Howard and starring Tom Hanks as Lovell, Bill Paxton as Haise, Kevin Bacon as Swigert, Gary Sinise as Mattingly, Ed Harris as flight director Gene Kranz, and Kathleen Quinlan as Marilyn Lovell. James Lovell, Eugene Kranz, and other principals have stated that this film depicted the events of the mission with reasonable accuracy, given that some dramatic license was taken. For example, the film changes the tense of Lovell's famous follow-up to Swigert's original words from, "Houston, we've had a problem" to "Houston, we have a problem". The film also invented the phrase "Failure is not an option". The film was nominated for several Academy Awards, including Best Picture, Best Supporting Actor (Harris) and Best Supporting Actress (Quinlan).
In the 1998 miniseries From the Earth to the Moon, co-produced by Hanks and Howard, the mission is dramatized in the episode "We Interrupt This Program". Rather than showing the incident from the crew's perspective as in the Apollo 13 feature film, it is instead presented from an Earth-bound perspective of television reporters competing for coverage of the event.
In 2008, an interactive theatrical show titled Apollo 13: Mission Control premiered at BATS Theatre in Wellington, New Zealand. The production faithfully recreated the mission control consoles and audience members became part of the storyline. The show also featured a "guest" astronaut each night: a member of the public who suited up and amongst other duties, stirred the oxygen tanks and said the line "Houston, we've had a problem." This "replacement" astronaut was a nod to Jack Swigert, who replaced Ken Mattingly shortly before the launch in 1970. The production toured to other cities extensively in New Zealand and Australia in 2010–2011. The production was scheduled to travel to the US in 2012.
In the DC's Legends of Tomorrow episode "Moonshot", the oxygen tank explosion is averted when Eobard Thawne disguises himself as Swigert, in order to retrieve a piece of the Spear of Destiny that was hidden in the pole section of the American flag planted on July 21, 1969. Thawne and Ray Palmer crash land the lander on the Moon's surface.
In November 2011, a notebook containing a checklist Lovell used to calculate a trajectory to get the damaged spacecraft, Apollo 13, back to Earth, and handwritten calculations by Lovell, was auctioned off by Heritage Auctions for $388,375. NASA made an email inquiry asking Heritage if Lovell had clear title to the notebook, stating that NASA had "nothing to indicate" the agency had ever transferred ownership of the checklist to Lovell. In January 2012, Heritage stated that the sale had been placed on hold after NASA launched an investigation into whether it was the astronaut's property to sell.
- Orloff, Richard W. (September 2004) [First published 2000]. "Table of Contents". Apollo by the Numbers: A Statistical Reference. NASA History Division, Office of Policy and Plans. NASA History Series. Washington, D.C.: NASA. ISBN 0-16-050631-X. LCCN 00061677. NASA SP-2000-4029. Retrieved April 15, 2012.
- Press Kit, pp. 108–109.
- "Astronaut Bio: John L. Swigert". NASA. January 1983. Archived from the original on July 31, 2009. Retrieved August 21, 2009.
- Press Kit, pp. 111–112.
- Slayton, Donald K. "Deke"; Cassutt, Michael (1994). Deke! U.S. Manned Space: From Mercury to the Shuttle (1st ed.). New York: Forge. p. 236. ISBN 0-312-85503-6.
- "Apollo 13 Crew". Smithsonian National Air and Space Museum. Retrieved January 6, 2018.
- "MSC 69–56" (PDF) (Press release). NASA. August 6, 1969. Retrieved July 27, 2019.
- Mission Operations Report Apollo 13 (PDF). Houston, TX: NASA. April 28, 1970. MSC-02680. Retrieved July 3, 2013.
- Kranz 2000, p. 307.
- Lovell, Kluger 1994, p. 79.
- Orloff & Harland, p. 362.
- "Mission insignias". NASA. Retrieved July 21, 2019.
- "Lumen Martin Winter – Kansapedia – Kansas Historical Society". www.kshs.org. Retrieved July 21, 2019.
- Chaikin, p. 291.
- Lovell, Kluger 1994, p. 87.
- Press Kit, p. 74.
- "Day 1: Earth orbit and translunar injection". Apollo Lunar Flight Journal. February 17, 2017. Retrieved July 28, 2019.
- Harland, p. 50.
- Orloff & Harland, p. 364.
- Press Kit, pp. 78, 81.
- Harland, p. 53.
- Harland, pp. 38–39.
- Press Kit, p. 29.
- Press Kit, p. 42.
- Press Kit, p. 33.
- Science News 1970-04-04, p. 354.
- Press Kit, p. 49.
- Press Kit, p. 51.
- Press Kit, p. 62.
- Press Kit, p. 65.
- Press Kit, pp. 33, 65.
- Press Kit, p. 73.
- Jones, Eric M. (February 20, 2006). "Commander's stripes". NASA. Retrieved July 20, 2019.
- Turnill, p. 316.
- Harland, p. 51.
- Harland, pp. 51–53.
- Press Kit, p. 104.
- Orloff & Harland, p. 363.
- Press Kit, p. 105.
- Jones, Eric M. (April 29, 2006). "Lunar Landing Training Vehicle NASA 952". Apollo Lunar Surface Journal. NASA. Retrieved July 20, 2019.
- "MSC 70–8" (PDF) (Press release). NASA. January 8, 1970. Retrieved July 27, 2019.
- Orloff & Harland, p. 385.
- "Apollo 13 mission: Science experiments". NASA. Retrieved August 8, 2019.
- Saturn 5 Launch Vehicle Flight Evaluation Report: AS-508 Apollo 13 Mission. George C. Marshall Space Flight Center. Huntsville, AL: NASA. June 20, 1970. MPR-SAT-FE-70-2. Retrieved May 30, 2017.
- Benson, Charles D.; Faherty, William Barnaby (1978). "Apollo 14 Launch Operations". Moonport: A History of Apollo Launch Facilities and Operations. NASA. NASA SP-4204. Retrieved July 3, 2013. Ch.22-7. Comments on Apollo 13 pogo.
- Fenwick, Jim (Spring 1992). "Pogo". Threshold. Pratt & Whitney Rocketdyne. Archived from the original on December 13, 2007. Retrieved July 3, 2013.
- Dotson, Kirk (Winter 2003–2004). "Mitigating Pogo on Liquid-Fueled Rockets" (PDF). Crosslink. El Segundo, CA: The Aerospace Corporation. 5 (1): 26–29. Retrieved July 3, 2013.
- Woods, W. David; Turhanov, Alexandr; Waugh, Lennox J., eds. (2016). "Launch and Reaching Earth Orbit". Apollo 13 Flight Journal. NASA. Retrieved August 5, 2019.
- Atkinson, Nancy (April 14, 2010). "13 things that saved Apollo 13, Part 5: Unexplained shutdown of the Saturn V center engine". Universe Today.
- "Day 1: Transposition, Docking and Extraction". Apollo Lunar Flight Journal. February 17, 2017. Retrieved August 12, 2019.
- Orloff & Harland, pp. 367.
- "Day 2: Midcourse correction 2 on TV". Apollo Lunar Flight Journal. February 17, 2017. Retrieved August 7, 2019.
- Gatland, Kenneth (1976). Manned Spacecraft (Second ed.). New York: MacMillan. p. 211. ISBN 0-02-542820-9.
- "NASA Apollo Mission Apollo-13". nasa.gov.
- Orloff, Richard W. (September 2004) [First published 2000]. "Apollo 13 Timeline". Apollo by the Numbers: A Statistical Reference. NASA History Division, Office of Policy and Plans. NASA History Series. Washington, D.C.: NASA. ISBN 0-16-050631-X. LCCN 00061677. NASA SP-2000-4029. Retrieved December 31, 2012.
- Page 4-44 Paragraph 2 https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19700076776.pdf
- Cortright, Edgar M. (June 15, 1970), Report of the Apollo 13 Review Board (PDF), Washington, D.C.: NASA Text (.TXT) file of report here. Multi-part PDF files of the report are available here Archived June 6, 2013, at the Wayback Machine and here Archived May 18, 2013, at the Wayback Machine.
- "Apollo 13 Command and Service Module (CSM)". National Space Science Data Center. NASA. Retrieved October 31, 2009.
- Lovell, Jim; Kluger, Jeffrey (2000) [Previously published 1994 as Lost Moon]. Apollo 13. Boston: Houghton Mifflin Company. pp. 83–87. ISBN 0-618-05665-3. LCCN 99089647.
- "Apollo 13 Lunar Module/ALSEP". National Space Science Data Center. NASA. Retrieved October 31, 2009.[dead link]
- Paterson, Chris. "Space Program and Television". Museum of Broadcast Communications. Archived from the original on December 4, 2010. Retrieved October 30, 2009.
- "AS13-62-8929". Apollo Imagery. NASA. April 11–17, 1970. NASA photo ID: AS13-62-8929; GRIN DataBase Number: GPN-2002-000056. Retrieved February 28, 2017.
- Barell, John (November 18, 2016). Antarctic Adventures: Life Lessons from Polar Explorers. Balboa Press. p. 154. ISBN 9781504366526. Retrieved February 28, 2017.
- Leopold, George (March 17, 2009). "Power engineer: Video interview with Apollo astronaut Ken Mattingly". EE Times. UMB Tech. Retrieved August 14, 2010.
- Siceloff, Steven (September 20, 2007). "Generation Constellation Learns about Apollo 13". Constellation Program. NASA. Retrieved December 31, 2012.
- "Bernard Etkin helped avert Apollo 13 tragedy". The Globe and Mail. Retrieved July 23, 2014.
- Pappalardo, Joe (May 1, 2007). "Did Ron Howard exaggerate the reentry scene in the movie Apollo 13?". Air & Space/Smithsonian. Washington, D.C.: Smithsonian Institution. Retrieved March 11, 2013.
- Lovell, James A. (1975). "Tired, Hungry, Wet, Cold, Dehydrated". In Cortright, Edgar M. (ed.). Apollo Expeditions to the Moon. Washington, D.C.: NASA. NASA SP-350. Retrieved July 4, 2013.
- "NASA Image and Video Library S70-17646". images.nasa.gov.
- Drushel, Richard F. (February 18, 2007). "Report of Apollo 13 Review Board PDF File (NASA) Restoration". Case Western Reserve University. Archived from the original on May 18, 2013. Retrieved July 4, 2013.
- Cortright, Edgar M. (June 15, 1970). "Report of Apollo 13 Review Board" (PDF). Washington, D.C.: NASA. Text (.TXT) file of report here. Multi-part PDF files of the report are available here Archived June 6, 2013, at the Wayback Machine and here Archived May 18, 2013, at the Wayback Machine. NASA's official report does not use the word "explosion" in describing the tank rupture. See findings 26 and 27 Archived October 15, 2012, at the Wayback Machine (PDF) on page 195 (5–22) of the NASA report.
- Williams, David R. "The Apollo 13 Accident". National Space Science Data Center. NASA. Retrieved December 31, 2012.
- Lovell, Jim; Kluger, Jeffrey (1994). Lost Moon: The Perilous Voyage of Apollo 13. Boston: Houghton Mifflin Company. pp. 349–50. ISBN 0-395-67029-2. LCCN 94028052.
- "Appendix E: CSM Electrical and Environmental Officer (EECOM)" (PDF). Mission Operations Report Apollo 13. Houston, TX: NASA. April 28, 1970. p. E-10. MSC-02680. Retrieved July 4, 2013.
- "Appendix H: LM Control Officer (Control)" (PDF). Mission Operations Report Apollo 13. Houston, TX: NASA. April 28, 1970. p. H-9. MSC-02680. Retrieved December 31, 2012.
- Gatland, Kenneth (1976). Manned Spacecraft (Second ed.). New York: MacMillan. p. 281. ISBN 0-02-542820-9.
- Glenday, Craig, ed. (2010). Guinness World Records 2010. New York: Bantam Books. p. 13. ISBN 978-0-553-59337-2.
- Lovell, James A. (1975). "'Houston, We've Had a Problem'". In Cortright, Edgar M. (ed.). Apollo Expeditions to the Moon. Washington, D.C.: NASA. NASA SP-350. Retrieved July 4, 2013.
- Shiflett, Kim (April 17, 2015). "Members of Apollo 13 Team Reflect on 'NASA's Finest Hour'". NASA. Retrieved June 16, 2018.
- Foerman, Paul; Thompson, Lacy, eds. (April 2010). "Apollo 13 – NASA's 'successful failure'" (PDF). Lagniappe. Hancock County, MS: John C. Stennis Space Center. 5 (4): 5–7. Retrieved July 4, 2013.
- Seil, Bill (July 5, 2005). "NASA's Finest Hour: Sy Liebergot recalls the race to save Apollo 13" (PDF). Boeing News Now. Boeing Company. Archived from the original (PDF) on April 9, 2012.
- "Behind the Scenes of Apollo 13". Richard Nixon Foundation. April 11, 2016. Retrieved June 27, 2019.
- "121 – Remarks on Presenting the Presidential Medal of Freedom to Apollo 13 Mission Operations Team in Houston". The American Presidency Project. Retrieved December 27, 2017.
- Karl D. Dodenhoff, RN. "Apollo Lunar Surface Experiment Package (ALSEP)". My Little Space Museum. Retrieved December 31, 2012.
- Dorr, Eugene. "The Artists". Space Mission Patches. Retrieved July 12, 2013.
- Dorr, Eugene. "Apollo 13". Space Mission Patches. Retrieved July 12, 2013.
- "Steeds Of Apollo". Lovell's of Lake Forest (Steakhouse). Lake Forest, IL. Archived from the original on January 22, 2012. Retrieved January 19, 2012.
- "Apollo 13 Mission: Science Experiments". Lunar and Planetary Institute. Universities Space Research Association. Retrieved July 4, 2013.
- Grabois, Michael R. "Apollo 13: the Towing Invoice". Archived from the original on October 31, 2007. Retrieved December 31, 2012.
- "Tongue-in-Cheek-Bill Asks Space Tow Fee". Spokane Daily Chronicle. April 18, 1970. p. 7. Retrieved July 4, 2013.
- KSC (February 11, 2011). "Raumfahrt mal nicht ganz so Ernst????". Raumcon Internet Forum. Raumfahrer.net. Retrieved July 4, 2013. One version of the invoice includes an extra $100,000 charge "for keeping this invoice confidential".
- "General Safety Considerations" (PDF lecture notes). Fusion Technology Institute, University of Wisconsin–Madison. Spring 2000.
- Flank, Lenny (October 12, 2013). "Chicago's Adler Planetarium: Photo Diary". Daily Kos. Retrieved January 12, 2015.
- ""A Life at Stake" Houston ... We've Got a Problem (TV Episode 1978) – IMDb". Internet Movie Database. Retrieved February 14, 2015.
- Lovell, Jim (1975). ""Houston, We've Had a Problem"". In Cortright, Edgar M. (ed.). Apollo Expeditions to the Moon: Chapter 13 (PDF). Washington D.C.: NASA. SP-350.
- Apollo 13 Technical Air-to-Ground Voice Transcription (PDF). Houston, TX: NASA. April 1970. p. 160. Archived (PDF) from the original on October 25, 2007. Retrieved October 4, 2007.
Houston, we've had a problem.
- "Apollo 13 (1995) – Trivia". Internet Movie Database. Retrieved May 23, 2009.
- Granath, Bob (April 17, 2015). "Members of Apollo 13 Team Reflect on 'NASA's Finest Hour'". NASA. Retrieved July 1, 2019.
- "APOLLO 13: Mission Control". New Zealand Entertainment and Events Corporation. Archived from the original on January 22, 2013. Retrieved December 31, 2012.
- "Apollo 13: Mission Control: Apollo 13 boldly goes where no theatre has gone before". The New Zealand Performing Arts Review & Directory. The Theatreview Trust. Retrieved July 4, 2013. Theatreview media release and subsequent reviews of the BATS Theatre production of Apollo 13: Mission Control.
- "Moonshot". IMDB. March 14, 2017.
- Klotz, Irene (January 6, 2012). "NASA Inquiry Stops Apollo 13 Notebook Sale". Discovery News. Silver Spring, MD: Discovery Communications. Archived from the original on January 7, 2012. Retrieved December 31, 2012.CS1 maint: Unfit url (link)
- Chaikin, Andrew (1998) . A Man on the Moon: The Voyages of the Apollo Astronauts. New York: Penguin Books. ISBN 978-0-14-024146-4.
- Driscoll, Everly (April 4, 1970). "Apollo 13 to the highlands". Science News. 97 (14): 353–355. doi:10.2307/3954891. JSTOR 3954891.(subscription required)
- Harland, David (1999). Exploring the Moon: The Apollo Expeditions. London; New York: Springer. ISBN 978-1-85233-099-6.
- Apollo 13 Press Kit (PDF). Washington, D.C.: NASA. 1970. 70-50.
- Orloff, Richard W.; Harland, David M. (2006). Apollo: The Definitive Sourcebook. Chichester, UK: Praxis Publishing Company. ISBN 978-0-387-30043-6.
- Turnill, Reginald (2003). The Moonlandings: An Eyewitness Account. Cambridge, UK; New York: Cambridge University Press. ISBN 978-0-521-03535-4.
- Kranz, Gene (2000). Failure Is Not an Option : Mission Control from Mercury to Apollo 13 and Beyond. Simon & Schuster. ISBN 0743200799.
- Lovell, Jim; Kluger, Jeffrey (1994). Lost Moon: The Perilous Voyage of Apollo 13. Houghton Mifflin. ISBN 0618056653. (The page numbers in the footnotes are for the 2000 edition of this book)
|Wikimedia Commons has media related to Apollo 13.|
|Wikiquote has quotations related to: Apollo 13|
- "Apollo 13" at Encyclopedia Astronautica
- "Apollo-13 (29") at NASA, summary of mission
- Cass, Stephen (April 1, 2005). "Apollo 13, We Have a Solution". IEEE Spectrum. New York: Institute of Electrical and Electronics Engineers: Part 1 of 3. Archived from the original on July 28, 2013. Retrieved July 5, 2013.
- Atkinson, Nancy (April 8, 2010). "13 Things that Saved Apollo 13". Universe Today. Retrieved April 25, 2012.
- Apollo 13 Press Kit (PDF), NASA, Release No. 70-50K, April 2, 1970
- The Apollo Spacecraft – A Chronology NASA SP-4009, vol. IV, pt. 3
- "Table 2-41. Apollo 13 Characteristics" from NASA Historical Data Book: Volume III: Programs and Projects 1969–1978 by Linda Neuman Ezell, NASA History Series, NASA SP-4012, (1988)
- "Apollo Program Summary Report" (PDF), NASA, JSC-09423, April 1975
- "Apollo 13: Lunar exploration experiments and photography summary" (Original mission as planned) (PDF) NASA, February 1970
- Apollo 13 Spacecraft Incident Investigation (PDF) NASA, June 1970
- Report of Apollo 13 Review Board, (PDF) NASA, June 1970
- "Apollo 13 Technical Air-to-Ground Voice Transcription" (PDF) NASA, April 1970
- "Space Educators' Handbook Apollo 13" at NASA
- "Gene Kranz Oral History Interview, Part 2" at C-SPAN; interview conducted April 28, 1999
- The short film Apollo 13 "Houston, We've Got a Problem" is available for free download at the Internet Archive
- "Apollo 13: LIFE With the Lovell Family During 'NASA's Finest Hour'" – slideshow by Life magazine
- "Apollo 13: NASA's Finest Hour" – slideshow by Life magazine at the Internet Archive
- "Apollo 13: Triumph on the Dark Side" is an episode of Man, Moment, Machine, a 2006 documentary series that aired on The History Channel
- Apollo 13: Failure is Not An Option documentary on YouTube
- "Apollo 13 transcripts on Spacelog"
- "Apollo 13 – 'Houston, we've had a problem'" Audio of the Apollo 13 mission during its first moments of trouble
- Complete post-flight press conference, April 21, 1970: Part 1 – Part 2