General & OtherComparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m² (350 Tamara A Smith![Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m² (350]()
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m² (350
Tamara A Smith
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“Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m² (350 ” by Tamara A…
Catalogue details
- Author
- Tamara A Smith
- Category
- General & Other
- Language
- English
- Source
- HathiTrust