Preliminary Design of an Additively Manufactured Aerospike Rocket Engine Utilizing Hydrogen Peroxide Transpiration Cooling

Research output: Contribution to book/Conference proceedings/Anthology/Report › Conference contribution › Contributed

Contributors

Details

Original languageEnglish
Title of host publication11th European Conference for Aeronautics and Space Sciences (EUCASS)
Place of PublicationRome
Number of pages9
Publication statusPublished - 1 Jul 2025
Peer-reviewedNo

External IDs

ORCID /0000-0002-5710-6530/work/207303858

Keywords