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NASA TN D-4392

Title:NASA TN D-4392
Alternate title:Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. III, Performance of first stage with inlet-feedpipe-manifold assembly
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Note:National Aeronautics and Space Administration ;, 1968
  
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Subject:Pump turbines -- Aerodynamics
Subject:Pump turbines -- Models
Subject:Pump turbines -- Testing
Subject:Rockets (Aeronautics)
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