| 摘要 |
The invention relates to aerospace engineering, in particular to arrangements or adaptations of the launch vehicles propulsion systems. In the proposed modular stage design boosters are clustered and stacked as rigid unified panels, and adjacent panels jointed in the modular stage with ability of its pivoting and fixing after being pivoted. Such design allows to avoid disordered falling of majority of the modular stage parts of the launch vehicle to decrease damage threat for population and household installations, and to create preconditions to ensure its integrity for re-use. |
