Space module designed to be deployed in space to form a space platform and associated space platform
A space module designed to be deployed in space to form a space platform, the space module being formed of a predetermined number of elements all having the same flat shape in an extension plane of the corresponding element, each element being of a predetermined type, with at least one element forming a payload.
1 . A space module deployed in space to form a space platform, the space module comprising a predetermined number of elements all having the same flat shape in an extension plane of the corresponding element, with at least one element forming a payload, at least some elements forming a plurality of solar panels arranged around the payload in a frontal plane, and at least some elements forming a plurality of radiators arranged substantially behind the payload in a second plane perpendicular to the frontal plane.
2 . The module according to claim 1 , wherein the first plane is oriented towards the Sun.
3 . The module according to claim 1 , wherein at least some of said elements comprise a plurality of radiators arranged in a second plane perpendicular to the first plane.
4 . The module according to claim 3 , wherein the second plane is aligned with the nadir of the Earth.
5 . The module according to claim 1 , wherein the flat shape is able to be inscribed in a circle presenting a cross-section of a loading compartment of a space launcher.
6 . The module according to claim 1 , wherein the flat shape presents identical dimensions for all the elements.
7 . The module according to claim 1 , wherein the payload comprises:
a data storage;
a processing server; and
a communicator communicating data with another space module of the same space platform and/or with an external communication station.
8 . The module according to claim 7 , wherein the payload further comprises a heat pump to dissipate heat.
9 . The module according to claim 1 , wherein each solar panel comprises:
a frame; and
a membrane stretched over this frame and presenting printed solar cells.
10 . The module according to claim 9 , wherein said frame is made of carbon-epoxy.
11 . The module according to claim 9 , wherein said membrane is comprised of polyetheretherketone (PEEK).
12 . The module according to claim 1 , wherein at least some of said elements are connected by connection interfaces, hinges, and/or springs.
13 . The module according to claim 1 , devoid of an energy storage device.
14 . A space platform comprising a plurality of modules according to claim 1 , the modules being assembled together.