Abstract
The side thruster is a highly responsive means for the attitude control of missiles. The sidejet force is influenced by the interaction between the sidejet and the air stream flow. This sidejet aerodynamic interaction effect was analyzed from following two view points: (1) the pressure field in the vicinity of the sidejet, (2) the force acting on the missile. Technical data of the sidejet interaction effect were obtained by means of flight tests of the missiles that were equipped with 4 impulse side thrusters which were small-size rapid burning solid propellant rocket motors. AIAA-98-4347
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
