Airship mounted array
A space-fed conformal array for a high altitude airship includes a primary array lens assembly adapted for conformal mounting to a non-planar airship surface. The lens assembly includes a first set of radiator elements and a second set of radiator elements, the first set and the second set spaced apart by a spacing distance. The first set of radiators faces outwardly from the airship surface to provide a radiating aperture. The second set of radiators faces inwardly toward an inner space of the airship, for illumination by a feed array spaced from the second set of radiators.
1. An array system for a high altitude airship, comprising:
a first primary array configured to mount to an exterior surface of an airship skin along a longitudinal flank of the airship;
a first feed array spaced from the first primary array and arranged to illuminate the first primary array;
a second primary array supported within an interior space of said airship and arranged generally transverse to a longitudinal axis of the airship; and
a second feed array spaced from the second primary array and arranged to illuminate the second primary array; and
wherein the second feed array is configured to mount to the exterior surface of the airship skin.
2. The array system of claim 1 , wherein said first and second primary arrays and said first and second feed arrays are configured to operate in a UHF frequency range.
3. The array system of claim 1 , wherein said first and second primary arrays and said first and second feed arrays are configured to operate in an X-band range.
4. The array system of claim 1 , wherein the airship has opposed first and second flanks on opposite sides of the inner space of the airship, and said first primary array is mounted on the first flank of the airship surface, and said first feed array is mounted on said second flank of the airship surface.
5. The array system of claim 1 , wherein said first primary array comprises a plurality of tile panels mounted conformally to the skin of the airship.
6. The array system of claim 1 , wherein the second primary array is mounted to an interior bulkhead of the airship.
7. The array system of claim 1 :
wherein the high altitude airship comprises an inflatable skin; and
wherein the airship skin comprises the inflatable skin.
8. The array system of claim 1 , wherein the first primary array comprises a first set of radiator elements and a second set of radiator elements, the first set and the second set being spaced apart by a spacing distance, the first set facing outwardly from the airship skin to form a radiating aperture, the second set facing inwardly toward an inner space of the airship.
9. The array system of claim 1 , wherein the first feed array comprises a plurality of rows of radiating elements to produce a feed pattern in an elevation plane, each row including a plurality of radiating elements, and having a longitudinal extent along the longitudinal axis of the airship.
10. The array system of claim 1 , wherein the first feed array is an elongated array with a longitudinal extent along the longitudinal axis of the airship.
11. The array system of claim 1 , wherein the first feed array is an active array.
12. The array system of claim 1 , wherein the second feed array is curved to conform to the exterior surface of the airship skin.
13. The array of claim 1 , wherein the airship has opposed first and second flanks on opposite sides of an inner space of the airship, and said first primary array is mounted on the first flank of the airship surface.
14. The array of claim 13 , wherein said first feed array is mounted on said second flank of the airship surface.
15. The array of claim 13 , wherein said first feed array is mounted in an upper area of the airship surface above an airship center.
16. The array of claim 13 , wherein said first feed array is mounted within said inner space of the airship.