CPC B64G 1/62 (2013.01) [B64G 5/00 (2013.01); B64G 2005/005 (2013.01)] | 14 Claims |
1. A method of stabilizing a landing rocket, comprising:
landing the rocket between a first stabilization element and a second stabilization element, wherein the first stabilization element is coupled to a first lateral support element and coupled to a second lateral support element spaced apart from the first lateral support element, and wherein the second stabilization element is coupled to the first lateral support element and coupled to the second lateral support element; and
moving the first stabilization element toward the second stabilization element.
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