| CPC B64B 1/42 (2013.01) | 20 Claims |

|
1. A water landing method for an aerospace vehicle, the method comprising:
descending with the aerospace vehicle, an axis of the aerospace vehicle aligned with a weight vector, the aerospace vehicle comprising a cabin with a cabin deck orthogonal to the axis;
contacting a surface of a body of water with a blunt nadir end of the aerospace vehicle along the axis;
decelerating the aerospace vehicle upon contact with the body of water; and
concurrently with decelerating the aerospace vehicle, flooding a fluid manifold between the blunt nadir end and a cabin with water from the body of water.
|