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    Apollo 16, LM-11 ascent propulsion system final flight evaluation (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The duty cycle for the LM-11 APS consisted of two firings, an ascent stage liftoff from the lunar surface, and the terminal phase initiation (TPI) burn. APS performance for the first firing was evaluated and found to be satisfactory. No propulsion data were received from the second APS burn; however, all indications were that the burn was nominal. Engine ignition for the APS lunar liftoff burn occured at the Apollo elapsed time (AET) of 175:31:47.9 (hours:minutes:seconds). Burn duration was 427.7 seconds.
    Keywords: SPACE SCIENCES
    Type: NASA-CR-134366 , MSC-07230-SUPPL-3 , TRW-20029-H162-RO-00
    Format: application/pdf
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