Composite structures for aerospace vehicles, and associated systems and methods
First Claim
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1. A space vehicle configured to contain at least one of crew or payload, the space vehicle comprising:
- a first septumized composite sandwich panel that forms a first outer wall portion of the space vehicle;
a second septumized composite sandwich panel that forms a second outer wall portion of the space vehicle, wherein each of the first and second septumized composite sandwich panels comprisesan outer face sheet that forms an exterior surface of the outer wall of the space vehicle;
an inner face sheet spaced apart from the outer face sheet;
at least one intermediate sheet disposed between the outer and inner face sheets;
a first core portion disposed between the outer face sheet and the intermediate sheet; and
a second core portion disposed between the inner face sheet and the intermediate sheet; and
a joint attaching the first septumized composite sandwich panel to the second septumized composite sandwich panel,wherein the outer face sheet and the first core portion of the first septumized composite sandwich panel define a first edge portion, and the inner face sheet, the second core portion and the intermediate sheet of the first septumized composite sandwich panel define a second edge portion offset from the first edge portion to form a first step,wherein the outer face sheet, the intermediate sheet, and the first core portion of the second septumized composite sandwich panel define a third edge portion, and the inner face sheet and the second core portion of the second septumized composite sandwich panel define a fourth edge portion offset from the third edge portion to form a second step, andwherein the first step faces the second step and the second edge portion is bonded to the third edge portion at the joint.
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Abstract
Composite structures for space vehicles and other aerospace vehicles are disclosed herein. In one embodiment of the disclosure, a space vehicle pressure vessel includes composite panels or sidewalls with septumized core. In another embodiment, a splice joint for joining septumized composite panels in space vehicle structures is disclosed herein.
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Citations
18 Claims
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1. A space vehicle configured to contain at least one of crew or payload, the space vehicle comprising:
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a first septumized composite sandwich panel that forms a first outer wall portion of the space vehicle; a second septumized composite sandwich panel that forms a second outer wall portion of the space vehicle, wherein each of the first and second septumized composite sandwich panels comprises an outer face sheet that forms an exterior surface of the outer wall of the space vehicle; an inner face sheet spaced apart from the outer face sheet; at least one intermediate sheet disposed between the outer and inner face sheets; a first core portion disposed between the outer face sheet and the intermediate sheet; and a second core portion disposed between the inner face sheet and the intermediate sheet; and a joint attaching the first septumized composite sandwich panel to the second septumized composite sandwich panel, wherein the outer face sheet and the first core portion of the first septumized composite sandwich panel define a first edge portion, and the inner face sheet, the second core portion and the intermediate sheet of the first septumized composite sandwich panel define a second edge portion offset from the first edge portion to form a first step, wherein the outer face sheet, the intermediate sheet, and the first core portion of the second septumized composite sandwich panel define a third edge portion, and the inner face sheet and the second core portion of the second septumized composite sandwich panel define a fourth edge portion offset from the third edge portion to form a second step, and wherein the first step faces the second step and the second edge portion is bonded to the third edge portion at the joint. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18)
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Specification