A numerical study has been performed to characterize the nozzle flow field of secondary
injection thrust vector control (SITVC) and to estimate the performance parameters of SITVC …

T= temperature t= time U= free stream velocity X= distance of the secondary nozzle axially
from the throat of the primary nozzle Xd= axial length of the divergent section of the primary …

The motive of this analysis is to compare the performance parameters of a single secondary
fuel injector and performance of Dual Secondary fuel injector system for Thrust Vector …

A thrust vectoring device contains four or more vanes placed in a cascade over the exit of a
nozzle to vector thrust and regulate the discharge throat area. A rod is included in the system …

HE noise regulations around the rocket launching stations due to the environmental concern
have made jet noise a crucial problem in the present day aero-acoustics research. Since the …