Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m²(350 psia) /

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Bibliographic Details
Main Author: Smith, Tamara A.
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Other Authors: Pavli, Albert J., Kacynski, Kenneth John
Format: Government Document Book
Language:English
Published: [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1987.
Series:NASA technical paper 2725.
Subjects: