Reliable flight computer for sounding rocket with dual redundancy: design and implementation based on COTS parts
Crossref DOI link: https://doi.org/10.1007/s13198-017-0584-x
Published Online: 2017-02-16
Published Print: 2017-09
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Kahe, Ghasem
License valid from 2017-02-16