NASA NTRS · 19700025214
Apollo 9 LM-3 ascent propulsion system, final flight evaluation
Abstract
Steady state performance analysis for ascent propulsion system during Apollo 9 mission burn to depletion
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Griffin, W. G., Thompson, P. F.. 1969-07-01. Apollo 9 LM-3 ascent propulsion system, final flight evaluation. https://ntrs.nasa.gov/citations/19700025214
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