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Wüstenberg, Henrik (2019) Estimation of Fuel Regression Rates in Hybrid Rocket Engines based on Pressure Measurement and Nozzle Throat Cross-section. Other.
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| Item URL in elib: | https://elib.dlr.de/132194/ | ||||||||
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| Document Type: | Thesis (Other) | ||||||||
| Additional Information: | Studienarbeit | ||||||||
| Title: | Estimation of Fuel Regression Rates in Hybrid Rocket Engines based on Pressure Measurement and Nozzle Throat Cross-section | ||||||||
| Authors: |
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| Date: | 26 November 2019 | ||||||||
| Refereed publication: | No | ||||||||
| Open Access: | No | ||||||||
| Number of Pages: | 123 | ||||||||
| Status: | Published | ||||||||
| Keywords: | hybrid rocket engine, hydrogen peroxide, hydroxyl-terminated polybutadiene, htpb, slab burner, regression rate, measurement method, data analysis, performance, combustion chamber model, nozzle erosion | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||
| HGF - Program: | Space | ||||||||
| HGF - Program Themes: | Space Transportation | ||||||||
| DLR - Research area: | Raumfahrt | ||||||||
| DLR - Program: | R RP - Space Transportation | ||||||||
| DLR - Research theme (Project): | Project ATEK (old) | ||||||||
| Location: | Braunschweig | ||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Spacecraft, BS | ||||||||
| Deposited By: | Passern, Silke | ||||||||
| Deposited On: | 07 Jan 2020 10:45 | ||||||||
| Last Modified: | 07 Jan 2020 10:45 |
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