초록 ▼

An inflatable aerodynamic deceleration method and system is provided for use with an atmospheric entry payload. The inflatable aerodynamic decelerator includes an inflatable envelope and an inflatant, wherein the inflatant is configured to fill the inflatable envelope to an inflated state such that

An inflatable aerodynamic deceleration method and system is provided for use with an atmospheric entry payload. The inflatable aerodynamic decelerator includes an inflatable envelope and an inflatant, wherein the inflatant is configured to fill the inflatable envelope to an inflated state such that the inflatable envelope surrounds the atmospheric entry payload, causing aerodynamic forces to decelerate the atmospheric entry payload.

대표청구항 ▼

1. An inflatable aerodynamic decelerator, comprising: an atmospheric entry payload having an exterior surface;an inflatable envelope configured to completely surround all of the exterior surface of the atmospheric entry payload when inflated; andan inflatant;wherein the inflatant is configured to fi

1. An inflatable aerodynamic decelerator, comprising: an atmospheric entry payload having an exterior surface;an inflatable envelope configured to completely surround all of the exterior surface of the atmospheric entry payload when inflated; andan inflatant;wherein the inflatant is configured to fill the inflatable envelope to an inflated state completely surrounding the atmospheric entry payload, causing aerodynamic forces to decelerate the atmospheric entry payload. 2. The inflatable aerodynamic decelerator of claim 1, further comprising restraining means configured to maintain the inflatable envelope and the atmospheric entry payload prior to inflation of the inflatable envelope. 3. The inflatable aerodynamic decelerator of claim 2, wherein the inflatant comprises a gas, the gas configured to fill the inflatable envelope to an inflated state subsequent to release of the restraining means. 4. The inflatable aerodynamic decelerator of claim 1, further comprising connecting means joining the atmospheric entry payload to the inflatable envelope when the inflatable envelope is in the inflated state. 5. The inflatable aerodynamic decelerator of claim 2, wherein the inflatant is a subliming solid placed within the inflatable envelope when in the restraining means. 6. The inflatable aerodynamic decelerator of claim 1, wherein the inflatant is a vaporizing liquid. 7. The inflatable aerodynamic decelerator of claim 1, wherein the inflatant is at least one reacting chemical configured to provide a gas. 8. The inflatable aerodynamic decelerator of claim 1, wherein the inflatant originates from a pressurized vessel. 9. The inflatable aerodynamic decelerator of claim 1, wherein the inflatant is introduced into the inflatable envelope prior to inflation of the inflatable envelope. 10. The inflatable aerodynamic decelerator of claim 2, wherein the inflatable envelope is encased in a reefing sleeve when inside the restraining means. 11. The inflatable aerodynamic decelerator of claim 10, wherein the reefing sleeve is configured to tear when the inflatable envelope is inflated. 12. The inflatable aerodynamic decelerator of claim 1, wherein the inflatable envelope is formed of a relatively thin material. 13. An apparatus, comprising: a payload having an exterior surface; andan inflatable envelope configured to be inflated to completely envelop all of the exterior surface of the payload using an inflatant;wherein the inflatant filling the inflatable envelope to an inflated state causes the inflatable envelope to completely surround the payload and aerodynamic forces to decelerate the atmospheric entry payload. 14. The apparatus of claim 13, further comprising connecting means joining the payload to the inflatable envelope when the inflatable envelope is in the inflated state. 15. The apparatus of claim 13, wherein the inflatant is a subliming solid initially located within the inflatable envelope. 16. The apparatus of claim 13, wherein the inflatant is a vaporizing liquid. 17. The inflatable aerodynamic decelerator of claim 1, wherein the inflatant is at least one reacting chemical configured to provide a gas. 18. The apparatus of claim 13, wherein the inflatant originates from a pressurized vessel. 19. The apparatus of claim 13, wherein the inflatant is introduced into the inflatable envelope prior to inflation of the inflatable envelope. 20. The apparatus of claim 13, wherein the inflatable envelope is initially encased in a reefing sleeve and folded and restrained by a restraining means. 21. The apparatus of claim 20, wherein the reefing sleeve is configured to tear away from the inflatable envelope when the inflatable envelope is inflated. 22. The apparatus of claim 17, wherein the inflatable envelope is formed of a relatively thin material. 23. The inflatable aerodynamic decelerator of claim 1, wherein a close-out panel forms a portion of the inflatable envelope that completely surrounds the exterior surface of the atmospheric entry payload.