Method for assemblying and landing a habitable structure on an extraterrestrial body
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0363346
(2006-02-28)
|
등록번호 |
US-7469864
(2008-12-30)
|
발명자
/ 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
1 인용 특허 :
8 |
초록
▼
A method for assembling and landing a habitable module on an extraterrestrial mass is claimed. At least one inflatable module and a second module are placed into orbit about an extraterrestrial mass. Connecting nodes, propulsion busses, and landing pads are also placed into orbit. A habitable struc
A method for assembling and landing a habitable module on an extraterrestrial mass is claimed. At least one inflatable module and a second module are placed into orbit about an extraterrestrial mass. Connecting nodes, propulsion busses, and landing pads are also placed into orbit. A habitable structure is constructed from the modules, busses, pads, and nodes. The structure can be robotically constructed. The habitable structure is then landed onto the surface of the extraterrestrial mass. The landing can be remotely controlled and the modules can be non-occupied.
대표청구항
▼
What is claimed is: 1. A method for assembling and landing a habitable structure having at least one inflatable module on an extraterrestrial mass, the method comprising the steps of: placing a substantially rigid space module into orbit about the extraterrestrial mass; placing an inflatable space
What is claimed is: 1. A method for assembling and landing a habitable structure having at least one inflatable module on an extraterrestrial mass, the method comprising the steps of: placing a substantially rigid space module into orbit about the extraterrestrial mass; placing an inflatable space module into orbit about the extraterrestrial mass; inflating the inflatable space module in space; placing at least one central node into orbit about the extraterrestrial mass; placing a plurality of propulsion buses into orbit about the extraterrestrial mass; placing a plurality of connecting nodes into orbit about the extraterrestrial mass; placing a plurality of landing pads into orbit about the extraterrestrial mass; constructing a habitable structure by connecting the substantially rigid space module to the central node, connecting the inflatable space module to the central node, attaching a connecting node to each propulsion bus and a connecting node being attached to an inflatable module, and a connecting node being attached to a substantially rigid module, and connecting a plurality of landing pads on each propulsion bus; and landing the habitable structure on the extraterrestrial mass by remotely controlling the plurality of propulsion busses and landing pads as the habitable structure approaches the surface of the extraterrestrial mass. 2. The method for landing a habitable structure on an extraterrestrial mass according to claim 1 wherein the extraterrestrial mass is the Moon. 3. The method for landing a habitable structure on an extraterrestrial mass according to claim 1 wherein the extraterrestrial mass is Mars. 4. The method for landing a habitable structure on an extraterrestrial mass according to claim 1 further including means for leveling the habitable structure. 5. The method for landing a habitable structure on an extraterrestrial mass according to claim 1 wherein the extraterrestrial mass is an asteroid. 6. A method for assembling and landing a habitable structure having an inflatable module, a substantially rigid space module, on an extraterrestrial mass, the method comprising the steps of: placing the substantially rigid space module into orbit about the extraterrestrial mass; placing at least one inflatable space module into orbit about the extraterrestrial mass; inflating the inflatable space module in space; placing at least one central node into orbit about the extraterrestrial mass; placing a plurality of propulsion buses into orbit about the extraterrestrial mass; placing a plurality of connecting nodes into orbit about the extraterrestrial mass; placing a plurality of landing pads into orbit about the extraterrestrial mass; constructing a habitable structure by connecting the substantially rigid space module to the central node, connecting the inflatable space module to the central node, attaching a connecting node to each propulsion bus a connecting node being attached to an inflatable module, and a connecting node being attached to a substantially rigid module, and connecting a plurality of landing pads on each propulsion bus; and landing the habitable structure on the extraterrestrial mass by remotely controlling the plurality of propulsion busses and landing pads as the habitable structure approaches the surface of the extraterrestrial mass. 7. The method for landing a habitable structure on an extraterrestrial mass according to claim 6 wherein the extraterrestrial mass is the Moon. 8. The method for landing a habitable structure on an extraterrestrial mass according to claim 6 wherein the extraterrestrial mass is Mars. 9. The method for landing a habitable structure on an extraterrestrial mass according to claim 6 further including means for leveling the habitable structure. 10. The method for landing a habitable structure on an extraterrestrial mass according to claim 6 wherein the extraterrestrial mass is an asteroid. 11. A method for assembling and landing a habitable structure having at least two inflatable modules on an extraterrestrial mass, the method comprising the steps of: placing at least two inflatable space modules into orbit about the extraterrestrial mass; inflating the inflatable space modules in space; placing at least one central node into orbit about the extraterrestrial mass; placing a plurality of propulsion buses into orbit about the extraterrestrial mass; placing a plurality of connecting nodes equal to the number of propulsion busses into orbit about the extraterrestrial mass; placing a plurality of landing pads into orbit about the extraterrestrial mass; constructing a habitable structure by connecting the inflatable space modules to the central node, attaching a connecting node to each propulsion bus and a connecting node being attached to each inflatable module, and connecting a plurality of landing pads on each propulsion bus; and landing the habitable structure on the extraterrestrial mass by remotely controlling the plurality of propulsion busses and landing pads as the habitable structure approaches the surface of the extraterrestrial mass. 12. The method for landing a habitable structure on an extraterrestrial mass according to claim 11 wherein the extraterrestrial mass is the Moon. 13. The method for landing a habitable structure on an extraterrestrial mass according to claim 11 wherein the extraterrestrial mass is Mars. 14. The method for landing a habitable structure on an extraterrestrial mass according to claim 11 further including means for leveling the habitable structure. 15. The method for landing a habitable structure on an extraterrestrial mass according to claim 11 wherein the extraterrestrial mass is an asteroid. 16. A method for assembling and landing a habitable structure having at least one inflatable module on an extraterrestrial mass, where the inflatable module, a second module, central node, at least two connecting nodes where each connecting node is attached to propulsion bus and each propulsion bus has a plurality of landing pads attached, are placed into orbit about an extraterrestrial mass, the method comprising the steps of: inflating the inflatable space module in space; constructing a habitable structure by connecting the second module to the central node, connecting the inflatable space module to the central node, attaching a connecting node to the inflatable module, and attaching a connecting node to the second module; and landing the habitable structure on the extraterrestrial mass by remotely controlling the plurality of propulsion busses and landing pads as the habitable structure approaches the surface of the extraterrestrial mass. 17. A method for assembling and landing a habitable structure on an extraterrestrial mass, the method comprising the steps of: placing an inflatable space module into orbit about the extraterrestrial mass; placing a second space module into orbit about the extraterrestrial mass; inflating the inflatable space module in space; placing at least one central node into orbit about the extraterrestrial mass; placing a first and second propulsion bus into orbit about the extraterrestrial mass; placing a first and second connecting node into orbit about the extraterrestrial mass; placing a plurality of landing pads into orbit about the extraterrestrial mass; constructing a habitable structure by connecting the inflatable space module to the central node, connecting the second space module to the central node, attaching the first connecting node to first propulsion bus, connecting the first connecting node to the inflatable space module, connecting the second propulsion bus to the second connecting node, connecting the second connecting node to the second space module, and connecting a plurality of landing pads on each propulsion bus; and landing the habitable structure on the extraterrestrial mass by remotely controlling the plurality of propulsion busses and landing pads as the habitable structure approaches the surface of the extraterrestrial mass.
이 특허에 인용된 특허 (8)
-
Soranno Kevin A. ; Younkin David L., Evolvable propulsion module.
-
Bigelow,Robert T.; Brian,Aiken, Flexible structural restraint layer for use with an inflatable modular structure.
-
Marshall,Manfred, Hydrogen-fueled spacecraft.
-
Thomas C. Taylor, Inflatable habitation volumes in space.
-
Bigelow, Robert T., Inflatable satellite bus.
-
Kawaguchi, Junichiro, Large membrane space structure and method for its deployment and expansion.
-
King Charles B. (Hampton VA) Hypes Warren D. (Toano VA) Simonsen Lisa C. (Yorktown VA) Butterfield Ansel J. (Newport News VA) Nealy John E. (Newport News VA) Hall ; Jr. John B. (Reston VA), Method of providing a lunar habitat from an external tank.
-
Cohen Marc M. (Palo Alto CA), Space station architecture, module, berthing hub, shell assembly, berthing mechanism and utility connection channel.
이 특허를 인용한 특허 (1)
-
White, Wayne Neville, Rapid assembly lightweight modular structure.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.