| 摘要 |
System comprising a test bed (1) and assembly (2, 4) comprising a divergent section (2) of a spacecraft motor, the assembly exhibiting the divergent section comprising a proximal end (41) and a distal end (22), the test bed (1) comprising a chassis (11) provided with means of fixing (12) the proximal end (41) of the assembly comprising the divergent section (2) to the chassis (11), the assembly being characterized in that the test bed (1) comprises actuators (3) adapted for applying loads locally to the divergent section (2), said loads simulating flight conditions of the divergent section (2). |
