Payload dispenser
A payload dispenser for a launch vehicle includes a plurality of panels. At least one panel includes a payload mounted onto the panel. The panels are attachable to each other to thereby form a self-supporting dispenser.
1. A self-supporting payload dispenser for a launch vehicle, comprising:
a first panel;
a second panel;
a third panel with a-payload mounted onto the third panel, wherein the payload comprises a satellite, wherein the first panel, the second panel, and the third panel are attachable to each other forming a self-supporting payload dispenser, wherein the self-supporting dispenser is a primary load bearing structure arranged to transfer loads from a launch vehicle to the payload, and is designed as a facetted tube with detachable sides.
2. The payload dispenser according to claim 1 , wherein the first panel comprises a second payload and the second panel comprises a third payload.
3. The payload dispenser according to claim 1 , wherein the first panel is free from any payload.
4. The payload dispenser according to claim 1 , wherein the payload dispenser extends in a longitudinal direction (X) and in a radial direction (R), wherein the first panel comprises a first attachment in the longitudinal direction (X) and the second panel comprises a second attachment in the longitudinal direction (X) which is attachable to the first attachment so that the first panel is attached to the second panel.
5. The payload dispenser according to claim 4 , wherein the first attachment and the second attachment are arranged to lock in position with relation to each other.
6. The payload dispenser according to claim 1 , wherein the payload dispenser extends in a longitudinal direction (X) and in a radial direction (R), and the payload dispenser is delimited in the radial direction (R) by the first panel, the second panel, and the third panel forming an envelope surface, wherein the first panel, the second panel, and the third panel are attachable to each other in an interface running in the longitudinal direction (X).
7. The payload dispenser according to claim 1 , wherein the payload dispenser is delimited in a lateral (Y) direction by the first panel, the second panel, and the third panel, wherein each of the first panel, the second panel, and the third panel extends in an unbroken manner in a longitudinal direction (X).
8. The payload dispenser according to claim 1 , wherein the first panel comprises panel portions attached to each other forming the first panel.
9. The payload dispenser according to claim 8 , wherein the panel portions are connected to each other in a longitudinal direction (X) and/or a lateral direction (Y).
10. The payload dispenser according to claim 9 , wherein the panel portions are fixedly attached to each other along laterally extending attachments.
11. The payload dispenser according to claim 1 , wherein the third panel comprises panel portions attached to each other forming the third panel.
12. The payload dispenser according to claim 11 , wherein the panel portions are connected to each other in a longitudinal direction (X) and/or a lateral direction (Y).
13. A method for assembly of a payload dispenser comprising:
a first panel;
a second panel;
a third panel with a payload mounted onto the third panel, wherein the payload comprises a satellite, and wherein the first panel, the second panel, and the third panel are attachable to each other forming a self-supporting payload dispenser, wherein the self-supporting dispenser is a primary load bearing structure arranged to transfer loads from a launch vehicle to the payload, and is designed as a facetted tube with detachable sides;
wherein the method of assembly comprises:
mounting a payload onto the third panel;
attaching the first panel and the second panel to each other via a first longitudinally extending attachment and a second longitudinally extending attachment;
locking the first attachment and the second attachment in position to hinder movement between the first panel and the second panel forming a self-supporting payload dispenser.
14. The method according to claim 13 , further comprising:
mounting a second payload onto the first panel before assembly of the first panel, the second panel, and the third panel; and
mounting a third payload onto the second panel before assembly of the first panel, the second panel, and the third panel.