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The Hypersonic Aerodynamic Characteristics of the Gemini Re-Entry Module Based on a Statistical Analysis of Wind Tunnel Test Data,
AEROSPACE CORP EL SEGUNDO CA EL SEGUNDO TECHNICAL OPERATIONS
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A set of hypersonic aerodynamic characteristics has been obtained for the Gemini re-entry module by a least squares curve fit of the appropriate ground test data to equation forms which are based on the related flow phenomena and simulation requirements.
APPROVED FOR PUBLIC RELEASE