Design, Development, Static and Flight Tests of Reverse Flow Multiple Nozzle Solid Rocket Motor with High Burn Rate Propellant

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Bibliographic Details
Published inCurrent science (Bangalore) Vol. 120; no. 1; p. 116
Main Authors Sreejith, K., Prasad, Shailesh, Bagavathiappan, R., Prasanth, C., Jeenu, R., Paul Murugan, J., Kurian, Thomas, Mansu, N., Harikrishnan, R., Levin, G., Eswaran, V.
Format Journal Article
LanguageEnglish
Published 10.01.2021
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ISSN:0011-3891
DOI:10.18520/cs/v120/i1/116-121