| 摘要 |
<p>The present invention relates to a hybrid thrust vector control system. The present invention comprises a Coanda surface installed on a discharge side of a thrust vector control nozzle, controlling the direction of thrust by using Coanda effect. As a result of the technical configuration of controlling the direction of thrust by movement of the Coanda surface without other control operation, the hybrid thrust vector control system can improve the efficiency of vector and reduce engine weight per thrust and maintenance costs due to a simplified drive system.</p> |
