Patents Assigned to Bigelow Development Aerospace
  • Publication number: 20160288927
    Abstract: A shield comprised of carbon nanotube materials is used to provide a level of protection to a spacecraft. Shield segments are produced in a facility in space. The segments are transported from the facility to a vicinity of a spacecraft hull. The segments are assembled over the hull to substantially cover an area of the hull.
    Type: Application
    Filed: March 28, 2016
    Publication date: October 6, 2016
    Applicant: Bigelow Development Aerospace
    Inventor: Robert T. Bigelow
  • Patent number: 6467221
    Abstract: The present invention provides an improved sleeping berth for space modules that can be expanded from a collapsed position to provide greater passenger comfort in a larger living space. The extension of the berth is accomplished using expandable gas inflated bellows between two hard surface housings. The berth can be retracted into its closed position simply by removing the air pressure from the bellows. The berth's retracted position may still accommodate a passenger and may be used in this position when space is unavailable for the berth's extension.
    Type: Grant
    Filed: August 23, 2000
    Date of Patent: October 22, 2002
    Assignee: Bigelow Development Aerospace
    Inventor: Robert T. Bigelow
  • Patent number: 6293500
    Abstract: The present invention provides an improved integrated translation tube for the movement of equipment and personnel through space modules, particularly for non-rigid type space modules such as the NASA Transhab module. In addition, the present invention provides an internal framework for the structural support of the space module itself, and the equipment installed internally to the space module. The present invention's arched shaped translation tube provides sufficient strength and rigidity to provide the required structural support, while simultaneously maximizing the uninterrupted interior volume of the space module.
    Type: Grant
    Filed: April 14, 2000
    Date of Patent: September 25, 2001
    Assignee: Bigelow Development Aerospace Division, Limited Liability Company
    Inventor: Robert T. Bigelow