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)/
| Main Author: | |
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| Corporate Authors: | , , |
| Other Authors: | , |
| Format: | Book |
| Language: | English |
| Published: |
Washington:
National Aeronautics and Space Administration, Scientific and Technical Information Office,
1987
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| Series: | NASA technical paper
2725 |
| Subjects: |