Aerospace balloon system and method of operation
A balloon system, preferably including a balloon and a payload. A balloon, preferably including a plurality of gores, a plurality of load members, and an apex fitting. A method of balloon system operation, preferably including deflating a balloon, and optionally including operating the balloon system in flight and/or landing the balloon system.
1. A system comprising:
a balloon comprising first balloon portion and a second balloon portion; and
an apex fitting comprising a first portion and a second portion, the first portion of the apex fitting connected to an apex end of the first balloon portion;
wherein, in a partially-inflated configuration of the system: the second balloon portion is mechanically connected to the first balloon portion via the second portion of the apex fitting and the apex fitting maintains a tension between the first and second balloon portions;
wherein the apex fitting is operable to transition the system from the partially-inflated configuration to a deflated configuration by: mechanically disconnecting the first portion of the apex fitting from the second portion of the apex fitting to release the tension.
2. The system of claim 1 , wherein mechanically disconnecting the first portion of the apex fitting from the second portion of the apex fitting comprises: at the apex fitting, releasing at least one of the first balloon portion or the second balloon portion.
3. The system of claim 1 , wherein the balloon defines a central axis between the apex and a nadir of the balloon, wherein the balloon further comprises a reinforcement portion encircling the central axis, wherein the first and second balloon portions are mechanically connected to the apex fitting via the reinforcement portion, wherein mechanically disconnecting the first portion of the apex fitting from the second portion of the apex fitting comprises severing the reinforcement portion proximal a boundary between the first and second balloon portions.
4. The system of claim 1 , wherein the apex fitting further comprises a blade, the blade operable to release the tension by severing a connection between the first and second portions of the apex fitting.
5. The system of claim 1 , wherein the balloon is a zero-pressure balloon.
6. The system of claim 1 , wherein, in the partially-inflated configuration, the balloon contains a lighter-than-air fluid.
7. The system of claim 1 , further comprising a payload, wherein, in the partially-inflated configuration and the deflated configuration, the payload is attached to the balloon.
8. The system of claim 1 , further comprising:
a payload; and
a nadir fitting at a nadir end of the balloon, wherein, in the partially-inflated configuration, the nadir fitting releasably tethers the payload to the balloon.
9. The system of claim 8 , further comprising a payload, wherein the apex fitting is operable to transition the system from the partially-inflated configuration to the deflated configuration while a projection of the balloon along a gravity vector does not intersect the payload.
10. The system of claim 1 , wherein the tension comprises a meridional tension.
11. A balloon system comprising:
a plurality of gores;
a plurality of load members connecting the plurality of gores, the plurality comprising a first set of load members and a second set of load members; and
an apex fitting comprising:
a first apex member attached to the first set of load members proximal an apex end; and
a second apex member attached to the second set of load members;
wherein, in a first configuration of the balloon system: the first apex member is mechanically connected to the second apex member, thereby mechanically coupling the first set of load members to the second set of load members;
wherein the apex fitting is operable to transition the balloon system from the first configuration to a second configuration by: detaching the first apex member from the second apex member to mechanically decouple the first and second sets of load members.
12. The balloon system of claim 11 , wherein the first set of load members is mechanically decoupled from the second set of load members by: at the apex fitting, releasing the second of load members.
13. The balloon system of claim 11 , wherein the apex fitting further comprises a blade, the blade configured to sever an attachment, wherein the attachment connects at least one of:
the first apex member to the second apex member,
the first apex member to the second set of load members, or
the first set of load members to the second set of load members.
14. The balloon system of claim 11 , wherein each gore of the plurality comprises a polymer film.
15. The balloon system of claim 11 , wherein, in the first configuration, the plurality of gores define a balloon envelope, wherein the plurality of gores contains a flammable lift gas within the balloon envelope.
16. The balloon system of claim 15 , wherein, in the second configuration, the flammable lift gas is vented from the balloon envelope.
17. The balloon system of claim 16 , wherein the flammable lift gas is vented substantially without atmospheric air mixing with the flammable vent gas within the balloon envelope.
18. The balloon system of claim 11 , wherein the balloon system is partially-inflated in the first configuration and deflated in the second configuration.
19. The balloon system of claim 11 , wherein a load member of the plurality carries a meridional tension in the first configuration, wherein the meridional tension is released in the second configuration.
20. The balloon system of claim 19 , wherein the load member comprises a load tape which seals a boundary between a pair of adjacent gores.