Burn rate characteristics of boron based solid propellant for ducted rocket applications
Crossref DOI link: https://doi.org/10.1007/s42401-025-00397-3
Published Online: 2025-08-13
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Kadiresh, P. N. https://orcid.org/0000-0002-8942-9270
Selvakumaran, T.
Balaji, K.
Text and Data Mining valid from 2025-08-13
Version of Record valid from 2025-08-13
Article History
Received: 23 April 2025
Revised: 26 July 2025
Accepted: 1 August 2025
First Online: 13 August 2025
Declarations
:
: The authors declare that they have no conflict of interest.