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 …

The fluid thrust vectoring is a technology that deflecting the main flow of an engine jet from
the centerline to transfer some force to the targeted axis through the primary and/or …

The pintle technology has been widely used in the aerospace vehicles and now it is an
active research topic in many industries to increase the range, speed and manoeuvrability of …

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 …

The use of pintle in rocket nozzles began in the early 1950s intending to solve the issues
associated with solid rocket propulsion. Uncontrolled combustion and thrust vectoring are …

The primary function of a rocket nozzle is to efficiently expand and accelerate the high-
speed exhaust gases from the combustion chamber. By adjusting the throat area of a …

Awp= throat area with pintle CFD= computational fluid dynamics D= outlet diameter L=
length of the nozzle NPR= nozzle pressure ratio P= static pressure Pe= exit pressure Pc …