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Latest revision Your text
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The closed fuel tank experiment involved pressurizing the hydrogen tank by closing its vents, while depressurizing the oxygen tank by allowing it to continue venting. It was expected that the pressure difference between the two tanks (measured as high as {{convert|39.4|psi|kPa}} would collapse the common bulkhead separating them, as happened in a ground test. The rupture occurred during the two-minute loss of signal between the [[Lyndon B. Johnson Space Center|Manned Spacecraft Center]] and the [[Trinidad]] [[Missile Test Project#Tracking stations|tracking station]]. The Trinidad radar image indicated the vehicle was in multiple pieces, and telemetry was never re-acquired. NASA concluded that a spark or impact must have ignited the propellants, causing an explosion.

The closed fuel tank experiment involved pressurizing the hydrogen tank by closing its vents, while depressurizing the oxygen tank by allowing it to continue venting. It was expected that the pressure difference between the two tanks (measured as high as {{convert|39.4|psi|kPa}} would collapse the common bulkhead separating them, as happened in a ground test. The rupture occurred during the two-minute loss of signal between the [[Lyndon B. Johnson Space Center|Manned Spacecraft Center]] and the [[Trinidad]] [[Missile Test Project#Tracking stations|tracking station]]. The Trinidad radar image indicated the vehicle was in multiple pieces, and telemetry was never re-acquired. NASA concluded that a spark or impact must have ignited the propellants, causing an explosion.



Despite the destruction of the stage, the mission was classified as a success, having achieved all of its primary objectives and validating the design concept of the restartable S-IVB-500 version. In September [[Douglas Aircraft Company]], which built the S-IVB, declared that the design was ready for use on the Saturn V to send men to the Moon.

Despite the destruction of the stage, the mission was classified as a success, having achieved all of its primary objectives and validating the design concept of the restartable S-IVB-500 version. In September [[Douglas Aircraft Company]], who built the S-IVB, declared that the design was ready for use on the Saturn V to send men to the Moon.



==References==

==References==

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