Pod for space or near-space flights

1. A pod for flights to and/or from space or near-space, comprising:

a pressurized body configured to host passengers therein,

said pressurized body having a substantially ring-like shape provided around a central axis and having a central opening, wherein

said pressurized body comprises an internal surface substantially facing said central axis, and an external surface substantially facing away from said central axis, and

wherein one or more windows are provided substantially along the part of said external surface furthest away from the central axis, and

wherein said substantially ring-like shape is a toroid;

wherein the non-pressurized body comprises a textile-based decelerator for descending, wherein said textile-based decelerator comprises a parafoil or a parachute.

2. A pod according to claim 1 , wherein said one or more windows are provided along at least approximately 25% of the external diameter of the pressurized body, or along at least 45% of the external diameter of the pressurized body, or along approximately 70% of the external diameter of the pressurized body.

3. A pod according to claim 1 , wherein the pod furthermore comprises a non-pressurized body connected to the pressurized body, wherein the connection between the pressurized body and the non-pressurized body comprises a motion damping structure.

4. A pod according to claim 3 , wherein the non-pressurized body comprises at least one guide and the pressurized body is arranged in such a way that it can perform a limited movement along said guide.

5. A pod according to claim 3 , wherein said non-pressurized body at least partially occupies the central opening of said pressurized body, said non-pressurized body houses at least one or more of: a radiator, cold plates, an antenna.

6. A pod according to claim 3 , wherein the non-pressurized body comprises one or more impact attenuators for absorbing an impact at landing, wherein said one or more impact attenuators comprise at least one airbag.

7. A pod according to claim 3 , wherein all systems relating to accelerating or decelerating the pod are connected to the non-pressurized body so that loads related to acceleration or deceleration are introduced into the pod via the non-pressurized body.

8. A pod according to claim 1 , wherein an outer structure of the pressurized body comprises a substantially rigid structure.

9. A pod according to claim 1 , wherein an outer structure of the pressurized body comprises a substantially flexible inflatable structure.

10. A pod according to claim 1 , wherein said pressurized body comprises a shape obtained by revolving a geometrical figure around an axis of revolution external to that figure, wherein said geometrical figure is a circle, such that the external shape of the pressurized body of the pod is a torus, or wherein said geometrical figure is an ellipse.

11. A pod according to claim 1 , wherein said pressurized body comprises a plurality of interconnected ring segments.

12. A vehicle for space or near-space flight comprising:

a detachable balloon that is detachable from the vehicle; and

a pod for flights to and/or from space or near-space, the pod comprising a pressurized body configured to host passengers therein,

said pressurized body having a substantially ring-like shape provided around a central axis and having a central opening, wherein

said pressurized body comprises one or more windows, and

said substantially ring-like shape is a toroid.

13. A vehicle according to claim 12 , wherein said balloon is filled with helium.

14. A vehicle according to claim 12 , further comprising a textile-based decelerator.

15. A vehicle according to claim 12 , wherein the pod furthermore comprises a non-pressurized body connected to the pressurized body, wherein said balloon is connected to the non-pressurized body.

16. A method of using a vehicle according to claim 12 comprising flying said vehicle to an altitude of between 30 km and 40 km.

17. The method of claim 16 , further comprising separating the balloon from the pod after the vehicle reaches a desired altitude, such that the vehicle does not include the balloon anymore.

18. The method of claim 17 , wherein after separating the balloon from the pod, the method further comprising descending the pod to Earth using a textile-based decelerator.

19. A pod for flights to and/or from space or near-space, comprising

a pressurized body configured to host passengers therein, said pressurized body having a substantially ring-like shape provided around a central axis and having a central opening; and

a non-pressurized body connected to the pressurized body, wherein the connection between the pressurized body and the non-pressurized body comprises a motion damping structure, and

wherein said substantially ring-like shape is a toroid;

wherein the non-pressurized body comprises a textile-based decelerator for descending, wherein said textile-based decelerator comprises a parafoil or a parachute.

20. A pod according to claim 19 , wherein the non-pressurized body comprises at least one guide and the pressurized body is arranged in such a way that it can perform a limited movement along said guide.

21. A pod according to claim 19 , wherein said non-pressurized body at least partially occupies the central opening of said pressurized body, said non-pressurized body houses at least one or more of the following: radiators, cold plates, antennas.

22. A pod according to claim 19 , wherein the non-pressurized body comprises one or more impact attenuators for absorbing an impact at landing, wherein said one or more impact attenuators comprise at least one airbag.

23. A pod according to claim 19 , wherein all systems relating to accelerating or decelerating the pod are connected to the non-pressurized body so that loads related to acceleration or deceleration are introduced into the pod via the non-pressurized body.

24. A pod according to claim 19 , wherein said pressurized body comprises a plurality of interconnected ring segments.