Patents by Inventor John V. Smolik

John V. Smolik has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 6053454
    Abstract: A modular payload support for placement in an enclosure defined by the sidewalls of a launch vehicle includes a central hub, a plurality of trusses, and a plurality of modular outer panels. Each of the trusses includes an inner edge secured to the hub and extends radially outward from the hub. Each of the trusses further includes an outer edge, and a modular outer panel is secured to each of the truss outer edges. Each modular outer panel is adapted for attachment to the vehicle sidewall, with each modular outer panel being sized to span the available distance between the truss outer edge and the vehicle sidewall. Each of the trusses is constructed of a number of layers or plies, so that the trusses may be tailored to meet strength and stiffness requirements of a contemplated application.
    Type: Grant
    Filed: September 4, 1998
    Date of Patent: April 25, 2000
    Assignee: Hughes Electronics Corporation
    Inventors: John V. Smolik, Spencer C. Ku, Andrew I. Mactavish, Mark A. Spiwak
  • Patent number: 4506852
    Abstract: An apparatus for launching a payload, such as a spacecraft or satellite, from a launch vehicle in which a single instrumentality is employed to simultaneously impart angular momentum about the center of mass of the payload and linear momentum in a direction along the axis of rotation.
    Type: Grant
    Filed: May 18, 1982
    Date of Patent: March 26, 1985
    Assignee: Hughes Aircraft Company
    Inventors: Gerald J. Adams, William L. Burkett, Jr., John V. Smolik
  • Patent number: 4290570
    Abstract: A spacecraft specifically adapted for launch from the space shuttle by means of a cradle having locking and ejection mechanisms mounted therein. The cradle fastens into the payload bay of the space shuttle and returns therewith for reuse in subsequent launches. The spacecraft mounts at three points to the cradle, and the cradle mounts at three points to the shuttle such that a plane through the attachment points passes through the roll axis of the spacecraft at approximately the center of mass thereof. The cradle utilizes the truss structure of the spacecraft to produce the required stiffness by providing a structural tie between the two ends and the bottom of the cradle. At launch, the spacecraft is ejected with both linear and angular momentum, the spin providing gyroscopic stability. The locking mechanisms in the cradle can be remotely controlled to relock the spacecraft to the cradle in the event of an unsuccessful deployment attempt.
    Type: Grant
    Filed: June 20, 1979
    Date of Patent: September 22, 1981
    Assignee: Hughes Aircraft Company
    Inventors: John V. Smolik, Ronald V. Swanson, Charles P. Rubin, James C. Blaschke, Roger J. Wagner