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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| Main Author: | |
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| Other Authors: | , |
| 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. |
| Subjects: |