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PROPELLANT VAPORIZATION AS A CRITERION FOR ROCKET-ENGINE DESIGN; EXPERIMENTAL PERFORMANCE, VAPORIZATION, AND HEAT-TRANSFER RATES WITH VARIOUS PROPELLANT COMBINATIONS [NASA MEMO 12-29-58E]

By: Clark, Bruce J.
Material type: materialTypeLabelBookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1959Description: 31p.
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