Anonymous asked in Science & MathematicsAstronomy & Space · 1 decade ago

what exactly failed on apollo 13 mission?

Summary or brief background about what failed on apollo 13 mission

5 Answers

  • 1 decade ago
    Favorite Answer

    Why don't you watch "Apollo 13" with Tom Hanks?

    Apollo 13

    Mission Summary

    The Apollo 13 mission was launched at 2:13 p.m. EST, April 11, 1970 from launch complex 39A at Kennedy Space Center. Apollo 13 Launch The space vehicle crew consisted of James A. Lovell, Jr. commander, John L. Swigert, Jr., command module pilot and Fred W. Haise, Jr. lunar module pilot.

    The Apollo 13 Mission was planned as a lunar landing mission but was aborted en route to the moon after about 56 hours of flight due to loss of service module cryogenic oxygen and consequent loss of capability to generate electrical power, to provide oxygen and to produce water.

    Spacecraft systems performance was nominal until the fans in cryogenic oxygen tank 2 were turned on at 55:53:18 ground elapsed time (GET). About 2 seconds after energizing the fan circuit, a short was indicated in the current from fuel cell 3, which was supplying power to cryogenic oxygen tank 2 fans. Within several additional seconds, two other shorted conditions occurred.

    Electrical shorts in the fan circuit ignited the wire insulation, causing temperature and pressure to increase within cryogenic oxygen tank 2. When pressure reached the cryogenic oxygen tank 2 relief valve full-flow conditions of 1008 psi, the pressure began decreasing for about 9 seconds, at which time the relief valve probably reseated, causing the pressure to rise again momentarily. About a quarter of a second later, a vibration disturbance was noted on the command module accelerometers.

    Damaged SMThe next series of events occurred within a fraction of a second between the accelerometer disturbances and the data loss. A tank line burst, because of heat, in the vacuum jacket pressurizing the annulus and, in turn, causing the blow-out plug on the vacuum jacket to rupture. Some mechanism in bay 4 combined with the oxygen buildup in that bay to cause a rapid pressure rise which resulted in separation of the outer panel. The panel struck one of the dishes of the high-gain antenna. The panel separation shock closed the fuel cell 1 and 3 oxygen reactant shut-off valves and several propellant and helium isolation valves in the reaction control system. Data were lost for about 1.8 seconds as the high-gain antenna switched from narrow beam to wide beam, because of the antenna being hit and damaged.

    As a result of these occurrences, the CM was powered down and the LM was configured to supply the necessary power and other consumables.

    The CSM was powered down at approximately 58:40 GET. The surge tank and repressurization package were isolated with approximately 860 psi residual pressure (approx. 6.5 lbs of oxygen total). The primary water glycol system was left with radiators bypassed.

    All LM systems performed satisfactorily in providing the necessary power and environmental control to the spacecraft. The requirement for lithium hydroxide to remove carbon dioxide from the spacecraft atmosphere was met by a combination of the CM and LM cartridges since the LM cartridges alone would not satisfy the total requirement. The crew, with direction from Mission Control, built an adapter for the CM cartridges to accept LM hoses.

    The service module was jettisoned at approximately 138 hours GET, and the crew observed and photographed the bay-4 area where the cryogenic tank anomaly had occurred. At this time, the crew remarked that the outer skin covering for bay-4 had been severely damaged, with a large portion missing. The LM was jettisoned about 1 hour before entry, which was performed nominally using primary guidance and navigation system.

  • Mark K
    Lv 6
    1 decade ago

    One of the fuel cells in the service module has an oxygen tank. During manufacture the tank was dropped by accident about 1&1/2 inches damaging a bleed valve. Also ,Beechcraft, a subcontracter, made a cryo stir fan at the wrong voltage ( they were not given an updated voltage memo from NASA) During a pre-launch test, the oxygen tank was filled,checked, and then they attempted to drain ity but couldn't because of the damaged valve. So they boiled off the oxygen by heating it. The tempatuires inside the tank climbed to over 1000 degrees F. unbeknowest to the techs

    boiling off the oxygen (their gauges did not go above 80 degrees). The high tempatures fused the wiring in the cryo fan.

    During the mission, Houston asked for a "cryo stir" and when the switch was thrown by the astronaut, the fused wiring caused a short cicuit and fire inside the insulated oxygen tank causing it to blow up severly damaging the service module with its life support systems.

  • Anonymous
    1 decade ago

    Basically, a wire had become frayed in one of the oxygen systems... When the astronauts (Fred Haise specifically) stirred the tanks, there was a spark generated because of the faulty wire which caused an oxygen tank to explode. This destroyed key systems on the spacecraft.

    For more information see the link below.

  • 1 decade ago

    the oxygen tanks exploded

    hope you r not superstitos about unlucky (13 its my lucky number)

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  • Anonymous
    1 decade ago

    the main problem was the number 13...they should have named it 12bis, 12# or something like that...

    better check it out yourself:

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