Abstract: Provided is a fabrication that is simple to make and cost effective in optimizing performance for moderately extended high velocity missions of high performance airborne vehicles. To counter rapid thermal loading while providing a relatively low cost structure, a laminate, in a preferred embodiment an intermediate modulus carbon fiber laminated as fabric layers in a resin matrix, is stitched through with glass fiber material. This laminate is then cured and formed as a section of skin of a supersonic missile, enabling extended supersonic operation, nominally some minutes after the laminate's Tg has been reached or exceeded. Additionally, an airframe and airframe members constructed in accordance with a preferred embodiment of the present invention are disclosed. Compared to existing materials, it reduces cost and weight, increases thermal stability, and maximizes internal payload.
Type:
Grant
Filed:
November 6, 2000
Date of Patent:
September 17, 2002
Assignee:
The United States of America as represented by the Secretary
of the Navy
Inventors:
Frank D. MacDonald, Patrick B. Stickler, Ryon C. Warren, Chun-Hua Kathy Chuang
Abstract: In a shooting range for training personnel in the use of firearms, a bullet trap that prevents rebounding bullets or flying debris from injuring shooters, has a central section of stacked cylindrical logs, or logs having a trapezoidal cross section, supported by stacked rectangular supporting blocks on each side. The stacked cylindrical logs have conical end sections at the end facing the shooter. These conical end sections direct incoming bullets to passageways between the cylindrical logs. Bullets passing through these passageways then strike a backstop panel. In a preferred embodiment, both the cylindrical logs and the backstop panel are made of shock-absorbing foamed fiber-reinforced concrete.
Type:
Grant
Filed:
March 5, 2001
Date of Patent:
September 10, 2002
Assignee:
The United States of America as represented by the Secretary
of the Army
Inventors:
Philip Garcin Malone, Charles Arthur Weiss, Jr., Brad Leslie Huntsman, Brent Elliot Huntsman
Abstract: Disclosed, in a preferred embodiment, is a switching circuit incorporating a Field Effect Transistor (FET), two series dual-tap gas tube surge arrestors, and high-voltage resistors as part of a high voltage switch of a fireset for initiating an exploding foil initiator (EFI). Until energizing the FET via a firing command, an operating voltage of 1000 V is held off by a combination of the surge arrestors and high-voltage resistors. Upon receipt of a firing signal, a 28 V source is used to energize the FET that, in turn, decreases the voltage across the one surge arrestor connected directly to ground and increases the voltage across the other surge arrestor. Upon reaching the breakdown voltage of the ionizable gas within the second surge arrestor, the gas ionizes, becomes electrically conductive, and dumps the second surge arrestor's voltage across the first surge arrestor. This causes the first surge arrestor to also break down. Both surge arrestors are now conducting.
Type:
Grant
Filed:
April 24, 2000
Date of Patent:
May 21, 2002
Assignee:
The United States of America as represented by the Secretary
of the Navy
Abstract: Provided is a compact, low-cost, lightweight, man-packable weapon system for engaging static and slowly maneuvering targets. In one embodiment, it may incorporate in its own backpack a compact launcher and multiple compact missiles, each weighing less than five pounds, for carry on a soldier's back. The missile itself uses a strapped-down acquisition and tracking sensor electrically connected to a simplified guidance system interfaced with an aero-control section capable of altering the flight path of the missile to a target. A solid-propellant rocket motor provides sufficient power to propel the missile at a predetermined limited speed and over a pre-determined limited distance that enables the proper operation of the simplified guidance system. A method for deploying a man-packable weapon system is disclosed also.
Type:
Grant
Filed:
June 7, 1999
Date of Patent:
June 12, 2001
Assignee:
The United States of America as represented by the Secretary
of the Navy