SUMMARY OF APOLLO AND LUNAR LOGISTICS SYSTEM PLANS UTILIZATION OF EXTRATERRESTRIAL RESOURCES SEMINAR PROCEEDINGS, SEPT. 25-26, 1962
Apollo project and lunar logistics system plans
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Apollo project and lunar logistics system plans
Axisymmetric external compression double cone inlet - mach 3 to 0.8 - pressure recovery, mass flow ratio, cowl pressure and additive drag
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Explore the source record for details and available documents.
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