Conceptio › Archive › DigitalCommons@USU
DigitalCommons@USUmetadata only

Nozzle Erosion Reconstruction Model for Data Analysis in Rocket Engines and Correlation With Chamber Pressure

Thibaudeau, Ryan J. et al.
DigitalCommons@USU · Papers
Open Source ↗
aerospace-engineering
graphite nozzle erosion, hybrid rocket propulsion, thrust coefficient, data reconstruction, chamber pressure, ground test analysis, nasa msfc, aerospace engineering
This document is indexed with metadata only — full text is not available in the archive for this record. Open the official source ↗
Record · ID 814158
Retrieved via Conceptio — every document is proof-bundled with source, license, and retrieval metadata.