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UID:launch-24756fd7-8ee6-431d-99f7-622d2b5683ce@padside
DTSTAMP:20260802T235150Z
DTSTART;VALUE=DATE:19680404
SUMMARY:Saturn V | Apollo 6
DESCRIPTION:Apollo 6 was intended to send a Command and Service Module (CS
 M) plus a Lunar Module Test Article (LTA)\, a simulated Lunar Module (LM)
  with mounted structural vibration sensors\, into a translunar trajectory
 . However\, the Moon would not be in position for a translunar flight\, a
 nd the Service Module engine would be fired about five minutes later to s
 low the craft\, dropping its apogee to 11\,989 nautical miles (22\,204 km
 ) and causing the CSM to return to Earth\, simulating a "direct-return" a
 bort. On
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