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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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.
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Series: | NASA technical paper
2725. |
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