Optimal two-stage parachute and retro motor sizing for launch vehicle stage recovery
Crossref DOI link: https://doi.org/10.1007/s12046-020-01420-3
Published Online: 2020-09-19
Published Print: 2020-12
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Priyadarshi, Pankaj http://orcid.org/0000-0001-9049-3678
Joseph, Leya
Saroha, Kamal
Text and Data Mining valid from 2020-09-19
Version of Record valid from 2020-09-19
Article History
Received: 27 March 2019
Revised: 9 December 2019
Accepted: 14 February 2020
First Online: 19 September 2020