CMD - Ceramic Stereolithography

Ceramic stereolithography (CSL) is a rapid prototyping and manufacturing process that use photocurable resin filled with a high loading of ceramic powder to produce ceramic parts using laser stereolithography machines. The parts produced by the stereolithography machine are in the green-state and are subsequently fired to achieve the desired ceramic properties.

 

Schematic of the Ceramic Stereolithography process

 

Fine Features, Intricate Geometry: The fine laser beam and the automated, layer-by-layer build approach of stereolithography enables ceramic parts with a high level of detail (fine features and complex geometry) that cannot be produced using conventional molding or machining methods.

 

Ceramic Stereolithographic part produced by TA&T, showing complex geometries

Ceramic Rapid Prototyping: Ceramic parts are built directly from a three dimensional CAD representation of the parts and do not require any part-specific tooling. This allows rapid, low-cost prototyping of fully-functional ceramic parts with the cost or leadtime associated with tooling.

 

A Gallery of example Ceramic Stereolithographically produce parts is available here.

 

TA&T offers Ceramic Prototyping Services using high purity alumina and fused silica materials

TA&T conducts Research and Development of new materials and applications for ceramic stereolithography.

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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