Experimental Investigation of a Gas Dynamic Thrust Vector Control for Hypersonic Space Planes.
Experimental Investigation of a Gas Dynamic Thrust Vector Control for Hypersonic Space Planes.
The feasibility and performance of a gas dynamic thrust vector control for advanced space planes using wall bleeding were investigated experimentally in the form of a parameter variation. In these studies, attempts were made to minimize the required control mass flows taken from the forebody boundary layer or intake. Furthermore, …