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UID:launch-24756fd7-8ee6-431d-99f7-622d2b5683ce@padside
DTSTAMP:20261016T132803Z
DTSTART;VALUE=DATE:19680404
SUMMARY:Saturn V | Apollo 6
DESCRIPTION:Apollo 6 was intended to send a Command and Service Module (CSM
 ) plus a Lunar Module Test Article (LTA)\, a simulated Lunar Module (LM) w
 ith mounted structural vibration sensors\, into a translunar trajectory. H
 owever\, the Moon would not be in position for a translunar flight\, and t
 he Service Module engine would be fired about five minutes later to slow t
 he craft\, dropping its apogee to 11\,989 nautical miles (22\,204 km) and 
 causing the CSM to return to Earth\, simulating a "direct-return" abort. O
 n
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