Open AccessDesign, Development, Static and Flight Tests of Reverse Flow Multiple Nozzle Solid Rocket Motor with High Burn Rate Propellant
Author(s) -
K. J. Sreejith,
S.V. Durga Prasad,
R. Bagavathiappan,
C. Prasanth,
R. Jeenu,
J. Paul Murugan,
Thomas Kurian,
N. Mansu,
R. Harikrishnan,
Г. Г. Левин,
V. Eswaran
Publication year - 2021
Publication title -
current science
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.281
H-Index - 118
ISSN - 0011-3891
DOI - 10.18520/cs/v120/i1/116-121
Subject(s) - propellant , nozzle , solid fuel rocket , aerospace engineering , burn rate (chemistry) , rocket engine nozzle , rocket (weapon) , aeronautics , flow (mathematics) , volumetric flow rate , chamber pressure , ballistics , environmental science , materials science , mechanics , nuclear engineering , automotive engineering , engineering , physics , projectile , metallurgy