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Please note that TD&E occured after the TLI burn, not before. The SPS engine on the Service Module did not have the thrust for the TLI burn for the CSM/LM stack and was only done on the unmanned Apollo 6 flight when the S-IVB failed to re-light itself after attainment of parking orbit.Rwboa22 (talk) 17:55, 30 July 2008 (UTC)