Patents by Inventor Elizabeth K. Bonderson

Elizabeth K. Bonderson 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: 11073366
    Abstract: A flare comprising an illuminant adjacent to a casing of a flare and a liner between the casing and the illuminant. The liner comprises a reaction product of a prepolymer and a curative, and one or more of a zinc oxide material or an aluminum oxide material. Methods of forming a flare are also disclosed.
    Type: Grant
    Filed: December 24, 2019
    Date of Patent: July 27, 2021
    Assignee: Northrop Grumman Systems Corporation
    Inventors: Robert S. Larson, Elizabeth K. Bonderson
  • Publication number: 20210190464
    Abstract: A flare comprising an illuminant adjacent to a casing of a flare and a liner between the casing and the illuminant. The liner comprises a reaction product of a prepolymer and a curative, and one or more of a zinc oxide material or an aluminum oxide material. Methods of forming a flare are also disclosed.
    Type: Application
    Filed: December 24, 2019
    Publication date: June 24, 2021
    Inventors: Robert S. Larson, Elizabeth K. Bonderson
  • Patent number: 9416217
    Abstract: A precursor formulation of a liner comprising a polymer and at least two curatives. One of the at least two curatives comprises a more reactive curative and the other of the at least two curatives comprises a less reactive curative. The more reactive curative is formulated to crosslink the polymer. A method of lining a rocket motor is also disclosed, as is a rocket motor including the liner.
    Type: Grant
    Filed: March 12, 2013
    Date of Patent: August 16, 2016
    Assignee: Orbital ATK, Inc.
    Inventors: Robert S. Larson, Elizabeth K. Bonderson
  • Publication number: 20140260184
    Abstract: A precursor formulation of a liner comprising a polymer and at least two curatives. One of the at least two curatives comprises a more reactive curative and the other of the at least two curatives comprises a less reactive curative. The more reactive curative is formulated to crosslink the polymer. A method of lining a rocket motor is also disclosed, as is a rocket motor including the liner.
    Type: Application
    Filed: March 12, 2013
    Publication date: September 18, 2014
    Applicant: ALLIANT TECHSYSTEMS INC.
    Inventors: Robert S. Larson, Elizabeth K. Bonderson
  • Patent number: 6054521
    Abstract: The present invention concerns an erosion resistant, low signature liner for solid propellant rocket motors and rocket motors having such a low signature liner. The liner combustion products in the exhaust plume have low visibility in the IR and visible light spectra which is essential for use in low signature solid propellant rocket motors. The liner also forms an in-situ protective layer at elevated temperatures for enhanced erosion resistance. These erosion resistant properties eliminate the need for supplemental case insulation which would contribute additional smoke and combustion products to the exhaust plume as well as add additional costs and inert weight to the motor.
    Type: Grant
    Filed: December 8, 1997
    Date of Patent: April 25, 2000
    Assignee: Cordant Technologies Inc.
    Inventors: Ronald W. Nelson, Merylin B. Lovett, Larry W. Poulter, Elizabeth K. Bonderson