Award Data

The overall abjective of this proposed project is the development of detailed definitions for the interfaces defined by the ABBET architecture. Signal models wil developed based upon the C/ATLAS set of signal nouns. A Test Foundation Framework (TFF) will be implemented to demonstrate the ability of test program or test program component transfer across multiple test platforms. This phase also w ...

For aircraft /store compatibility, a comprehensive software system requested by the Air Force for rapid assessment of flutter and ejection loads (RAFEL) poses challenging requirements. With ZAERO aeroelastic software as a base, ZONA can establish a RAFELsystem satisfying all AF's requirements. Specifically, ZONA will develop RAFEL in Phase I with: a) solution accuracy with flutter solution robustn ...

It is proposed to development of a large-scale production apparatus that produces single-walled carbon nanotubes (SWNT) and catalytic multi-walled nanotubes (MWNT) on a continuous process basis. A novel and flexible reactor design will be investigated. Theproposed reactor design will allow the control of production parameters including catalyst type and particle size, the type of carbon source, ca ...

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THE PROPOSED PROJECT WILL DETERMINE THE FEASIBILITY OF THE USE OF ADVANCED TYPE II FLUIDS FOR THE DE-ICING/ANTI-ICING OF GENERAL AVIATION (GA) AIRCRAFT WITH TAKEOFF SAFETY SPEEDS (V2) OF GENERALLY LESS THAN 85 KNOTS. TYPE II FLUIDS WILL BE APPLIED TO SEVERAL GA CATEGORY AIRCRAFT. THE ICE PROTECTION CAPABILITY OF THE FLUID WILL BE EVALUATED FOR DIFFERENT FREEZING PRECIPITATION CONDITIONS. THE EFFEC ...

The objective of this program is to develop an integrated tribology system for advanced low heat rejection (LHR) diesel engines. The system will consist of a substantially improved high-temperature liquid lubricant, for long life under severe conditions; improved compatible engine tribomaterials; and an on-board sensor arrays for direct monitoring of engine oil condition. Surfaces Research lubri ...

Proposed enhancement of the thermal control of rocket engine combustion chambers is achieved by implementing advanced high thermal conductivity, light weight polycapillary materials (APM) to provide improved transpiration cooling of the walls and/ordevelop efficient ablative chamber wall material. MER Corporation has developed the method of fabricating metal and/or ceramic APM characterized by ...

Fastening and joining technology has lagged behind the progress that has been made in other areas of composites for advanced air vehicles. Aerotech proposes the development of reversible polymeric adhesive bonding of composites using variable frequency microwave energy. With this method, composites are bonded using Poly Ether Ether Ketone (a high temperature thermoplastic) which is cured using v ...

Affordable/low cost carbon-carbon (C-C) composites are enabling to a number of defense, aerospace and commercial applications. However, in addition to cost, their limitation is carbon gasification in oxidative environments above about 750¿F (=400¿C). An inhibited carbon matrix that reduces oxidation rate by a factor of 200 with up to double the strength of uninhibited composites which could be ...

Affordable/low cost carbon-carbon (C-C) composites are enabling to a number of defense, aerospace and commercial applications. However, in addition to cost, their limitation is carbon gasification in oxidative environments above about 750¿F (=400¿C). An inhibited carbon matrix that reduces oxidation rate by a factor of 200 with up to double the strength of uninhibited composites which could be ...