Paper information

Paper code

IAC-26,C4,IP,48,x114285

Room

IP Area

Title

End-to-End Transient Simulation and Experimental Validation of a Nitrous Oxide Feed Line for a Lab-Scale Hybrid Rocket Motor

abstract

View PDF

Session

IP. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

symposium

C4. IAF SPACE PROPULSION SYMPOSIUM

congress

IAC-26

Type of presentation

interactive

Main author

Ms. Rukiyye Melek AYDURMUŞ, Gebze Technical University, Türkiye

Co-authors

Mr. Osman Giray Oguzman, Gebze Technical University, Türkiye;

Mr. Ahmet Arif Durhan, Istanbul Technical University, Türkiye;

Ms. Fatıme Sevgili, Gebze Technical University, Türkiye;

Mr. Hüseyin İlkutlu, Gebze Technical University, Türkiye;

Mr. Mert Tuna Albayrak, Türkiye;