Spinel - Transparent Armor

Technology Assessment & Transfer has developed Spinel transparent armor manufacturing to a point that makes it more affordable than ever before.  Windows can routinely be manufactured over a large range of sizes to near net shape specifications which minimizes Spinel powder consumption while simultaneously reducing grinding and finishing costs.  The armor blank fabrication process is also capable of producing curved windows.

Benefits of Transparent Spinel Armor

  • Improved ballistic performance solutions that are half the weight and thickness of traditional ballistic glass armor
  • Unique fracture patterns for increased multi-hit capability
  • High hardness for increased threat erosion capability as well as increased resistance to environmental abrasion and impact
  • Greater percentage of mid-wave IR transmission for increased NVG performance

TA&T Spinel windows have been successfully produced for the army to mount on FMTV demonstrator vehicles for evaluation at TARDEC.   Working under a DARPA contract TA&T has developed an ultra-lightweight armor solutions specifically tailored to Spinel performance thereby furthering its performance advantage over ballistic glass and other transparent ceramics.

TA&T has commercialized its hot pressed transparent armor manufacturing process through an exclusive licensing agreement with ArmorLine Corporation, a business unit of Defense Venture Group, located in Indian Land, SC.

 

Spinel Armor Defeats Barrett .50 Caliber - Twice


Ta&T news

TA&T Ceramic Stereolithographically Produced Parts Integral to Instrument Package on NASA Mars Science Laboratory’s Curiosity Rover

Annapolis, MD – November 29, 2011 – Ceramic Stereolithography (CSL), a unique manufacturing process developed by Technology Assessment and Transfer, Inc. (TA&T) under multiple SBIR and internally funded programs, was used to make ceramic heater bodies that are onboard the recently launched Mars rover named Curiosity.


Contracted by the NASA Goddard Space Flight Center, TA&T fabricated alumina pyrolysis oven housings that are being used in the Sample Analysis at Mars (SAM) suite of instruments. Patrick Jordan, a NASA engineer, explained that due to the complex nature of the housing, traditional machining of the ceramic was too expensive to undertake. The major impediment to machining the housing is a series of 52 closely spaced, small diameter (.012”) holes through which heating elements are placed. Impressively, the CSL process was able to create fully functional prototypes that survived the rapid heating to >1,000°C. The parts passed thermal shock and thermal cycle durability testing, and will be used on Mars to heat soil samples to determine the presence of water and organic compounds that indicate the possibility of life on Mars.


The CSL process has applications beyond space exploration, including those which have consumer and industrial applications. The process requires no tooling and therefore allows rapid prototyping of fully-functional ceramic parts. TA&T has been involved in the development of rocket engine fuel injectors, heat exchangers for cooling electronics in hybrid electric vehicles, ceramic molds for turbine engine blades, and electrosurgical medical device tips, among other development projects.


Photographs of the TA&T produced ceramic heater housing for the Mars Science Laboratory can be found in the Ceramic Stereolithography gallery.

 

Additional information about the Mars Science Laboratory mission can be found at http://www.nasa.gov/mission_pages/msl/index.html.

 

TA&T Completes Air Force SBIR Phase II Kickoff Meetings

Annapolis, MD – November 21, 2011 – Technology Assessment & Transfer, Inc. has just completed a kickoff meeting as a prime contractor on an Air Force SBIR Phase II.

 

Led by Dr. James Hom, the Air Force Phase II effort is focused on advanced cooling and packaging designs for electronic components within an aircraft's power electronic converter. The proposed component level solutions substantially reduce the thermal resistances between the highest heat producing components (e.g., the power switching modules, magnetic inductors, and capacitors) and the coolant. These solutions will be integrated into an existing power electronic converter and tested in a simulated aircraft environment. An increase in maximum allowable inlet coolant temperature of at least 30°C is expected.

 

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Spinel & Optical Ceramics
215 Najoles Road
Millersville, MD 21108
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Dr. Larry Fehrenbacher, President
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Sharon Fehrenbacher, CEO
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