Spacecraft heat shield
Spacecraft Heat Shield A deployable spacecraft atmospheric-entry heat shield ( 30, 40, 50, 60 ) is configured in a flasher pattern with a transformable polyhedral-surface. The transformable polyhedral-surface has a plurality of sectors ( 2 , see FIG. 1 a ), each sector ( 2 ) having a plurality of mountain fold lines ( 4, 5 ), a plurality of valley fold lines ( 6, 7 ), a plurality of facets ( 8 ) lying between the fold lines ( 4, 5, 6, 7 ) and an outside edge ( 12 ). The heat shield ( 30, 40, 50, 60 ) is configured to unfold from a stowed configuration to a deployed configuration.
1. A deployable spacecraft atmospheric-entry heat shield having a transformable polyhedral-surface comprising:
a polygon central region of order m; and
a plurality of sectors disposed around the central region, each sector having a plurality of mountain fold lines, a plurality of valley fold lines, a plurality of facets lying between the fold lines, and an outside edge,
wherein:
the plurality of mountain fold lines comprise a plurality of major mountain fold lines and minor mountain fold lines;
the plurality of valley fold lines comprise a plurality of major valley fold lines and minor valley fold lines;
the major mountain fold lines and the major valley fold lines extend from the central region to the outside edge;
the heat shield is configured to unfold from a stowed configuration to a deployed configuration,
the transformable polyhedral-surface is configured to adopt a swept back form in the deployed configuration; and
the major mountain fold lines have a swept back angle that is substantially constant from the polygon central region to the outside edge in the deployed configuration.
2. The heat shield of claim 1 , wherein the heat shield is a radiative heat shield.
3. The heat shield of claim 1 , wherein the minor mountain fold lines and the minor valley fold lines extend between the major mountain fold lines and the major valley fold lines.
4. The heat shield of claim 1 , wherein the transformable polyhedral-surface comprises a radial symmetry of order m about the polygon central region, wherein the plurality of sectors are radially symmetrical.
5. The heat shield of claim 1 , wherein a surface of the heat shield is formed as an integral sheet material.
6. The heat shield of claim 1 , wherein the plurality of fold lines of each sector are configured to substantially restrict angular rotation about a longitudinal axis of the heat shield in use.
7. The heat shield of claim 1 , wherein the ratio between a diameter of the polygon central region and an outer flat-diameter of the deployed configuration of the transformable polyhedral-surface is 1:11.
8. The heat shield of claim 1 , wherein the deployed configuration is configured such that the centre of mass of the heat shield is behind the polygon central region with respect to the normal of a longitudinal axis of the heat shield.
9. The heat shield of claim 1 , wherein the deployed configuration is a stable state and a retaining means is configured to maintain the heat shield in the stowed configuration.
10. The heat shield of claim 9 , wherein the retaining means is configured to release when an activation threshold is exceeded.
11. A spacecraft comprising a heat shield having a transformable polyhedral-surface comprising:
a polygon central region of order m; and
a plurality of sectors disposed around the central region, each sector having a plurality of mountain fold lines, a plurality of valley fold lines, a plurality of facets lying between the fold lines, and an outside edge,
wherein:
the plurality of mountain fold lines comprise a plurality of major mountain fold lines and minor mountain fold lines;
the plurality of valley fold lines comprise a plurality of major valley fold lines and minor valley fold lines;
the major mountain fold lines and the major valley fold lines extend from the central region to the outside edge;
the heat shield is configured to unfold from a stowed configuration to a deployed configuration;
the transformable polyhedral-surface is configured to adopt a swept back form in the deployed configuration; and
the major mountain fold lines have a swept back angle that is substantially constant from the polygon central region to the outside edge in the deployed configuration.