Granted Patent B2

US 12,371,919 · App. 18/334,104 · Granted Jul 29, 2025

Inventors: Joel C. Sercel (Lake View Terrace, CA); James G. Small (Sonoita, AZ); Philip J. Wahl (Alta Dena, CA); Craig E. Peterson (Los Angeles, CA)

Assignee: Trans Astronautica Corporation

E04H12/00E04B1/343B64G1/2227

Abstract

Claims (30)

1. An inflatable tower configured for Lunar deployment, comprising:

a payload platform configured to support a payload;

a membrane configured to be inflated to support the payload platform; and

a compressed gas canister configured to inflate the membrane to a pressure that is less than a threshold pressure at which a rate of leakage from one or more small holes in the membrane caused by micrometeor impacts can be compensated for by the compressed gas canister providing additional gas to the membrane, the threshold pressure resulting in the rate of leakage from the one or more small holes in the membrane that is compensated for by the compressed gas canister.

2. The inflatable tower of claim 1 , wherein the threshold pressure is about 100 Pa.

3. A method of deploying an inflatable tower on the Moon, comprising:

packaging a membrane of the inflatable tower in a deflated condition;

transporting the inflatable tower to a location on the Moon for deployment; and

delivering gas into the membrane to inflate the membrane and lift a payload platform to a top of the inflatable tower.

4. The method of claim 3 , wherein packaging the membrane comprises rolling the membrane onto one or more cylinders.

5. The method of claim 3 , wherein packaging the membrane comprises folding the membrane into a package.

6. A method of inflating an inflatable tower on the Moon, comprising:

placing the inflatable tower at a location on the Moon for deployment, the inflatable tower comprising a payload platform configured to support a payload at a top of the inflatable tower and a membrane configured to be inflated to support the payload platform;

inflating the membrane of the inflatable tower beginning at the top of the inflatable tower; and

progressively inflating lower sections of the inflatable tower after beginning inflation at the top of the inflatable tower.

7. A method of manufacturing an inflatable tower on the Moon, comprising:

extruding a membrane at a site for deploying the inflatable tower;

attaching the membrane to a payload platform; and

inflating the membrane to raise the payload platform to a raised position above a surface of the site.

8. The inflatable tower of claim 1 , wherein the compressed gas canister is attached to an upper surface of the tower.

9. The inflatable tower of claim 1 , wherein the threshold pressure is further selected such that circumferential hoop-stress levels in pressure-containing walls of the membrane are less than approximately half a maximum hoop-stress level for the membrane.

10. The inflatable tower of claim 1 , wherein the gas is chosen to have a sufficiently low boiling temperature at the threshold pressure such that the gas will not condense to a liquid or solid within an expected range of Lunar temperatures.

11. The method of claim 4 , wherein delivering gas into the membrane comprises:

introducing the gas a lower end cap coupled to a lower end of the membrane of the inflatable tower to provide a pneumatic pressure on one or more cylinders, the one or more cylinders located at an upper end of the membrane of the inflatable tower, the pneumatic pressure pushing the one or more cylinders upwards as the membrane is inflated.

12. The method of claim 4 , wherein the rolling the membrane onto one or more cylinders is performed in a vacuum chamber.

13. The method of claim 6 , wherein the inflatable tower is cone-shaped with a wider base than the top of the inflatable tower.

14. The method of claim 6 , wherein the sections of the inflatable tower are connected with a plurality of horizontal diaphragms, each of the horizontal diaphragms including a valve.

15. The method of claim 14 , wherein progressively inflating the lower sections comprises progressively opening the valves after beginning inflation at the top of the inflatable tower.

16. The method of claim 14 , wherein each of the valve comprise a pop-off valve configured to automatically open when a pressure difference between opposing ends of the pop-off valve exceeds a set value.

17. The method of claim 6 , wherein inflating the membrane of the inflatable tower is performed with a payload on the payload platform.

Assignments (1)

Continuity (4)

References Cited (258)