REFRACTORY COMPOSITES, INC.

Company Information

Company Name
REFRACTORY COMPOSITES, INC.
Address
107 N. Langley Rd.
Glen Burnie, MD, 21060
Phone
1 410-768-2490
URL
n/a
DUNS
n/a
Number of Employees
n/a

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$2,068,300.00
32
SBIR Phase II
$3,903,882.00
7
Chart code to be here

Award List

  1. TAILORABLE HIGH THERMAL CONDUCTIVITY CTE MATCHED COMPOSITE CERAMIC CIRCUIT BOARDS

    Amount: $49,914.00

    THIS PHASE I PROGRAM WILL DEMONSTRATE THE TECHNICAL VIABILITY OF DESIGNING AND MANUFACTURING INTEGRATED CERAMIC MATRIX COMPOSITE CIRCUIT BOARDS FOR A VARIETY OF ELECTRONIC DEVICES INCLUDING (HIGH POWE ...

    SBIR Phase I 1987 NavyDepartment of Defense
  2. HAFNIUM DIBORIDE MATRIX CERAMIC COMPOSITES FOR HYPERSONIC LEADING EDGE STRUCTURES

    Amount: $38,475.00

    REFRACTORY COMPOSITES, INC. PROPOSES TO CHEMICALLY VAPOR INFILTRATE HFB2 INTO A GRAPHITE FIBER STRUCTURE. INITIAL PROCESS EVALUATION TRIALS WILL BE FOLLOWED BY FLAT LAMINATE AND FOR .030 INCH RADIUS E ...

    SBIR Phase I 1987 NavyDepartment of Defense
  3. HIGH CHAR YIELD POLYMER MATRIX COMPOSITES

    Amount: $49,885.00

    STATE-OF-THE-ART CARBON-CARBON COMPOSITE PROCESSING GENERALLY EMPLOYS PYROLIZED PHENOLIC, FUFERAL, PITCH OR COMBINATIONS OF THESE MATERIALS AS MATRIX MATERIALS. BECAUSE THE CHAR YIELD IS IN THE 50% RA ...

    SBIR Phase I 1988 NavyDepartment of Defense
  4. CERAMIC COMPOSITE FASTENERS WITH METALLIC THREAD ZONES

    Amount: $49,477.00

    RCI PROPOSES TO COMBINE REFRACTORY METAL CVD TECHNOLOGIES AND CVI CERAMIC AND CARBON-CARBON COMPOSITE TECHNOLOGIES TO PRODUCE SMALL DIAMETER FASTENERS WITH METALLIC THREAD ZONES. THESE FASTENERS ARE E ...

    SBIR Phase I 1989 Air ForceDepartment of Defense
  5. CERAMIC MATRIX COMPOSITE HYPERSONIC ENGINE STRUCTURES

    Amount: $49,927.00

    ADVANCED COMPOSITES BASED ON CERAMIC OR CARBON MATRICES ARE CANDIDATES FOR HOT ENGINE WALL STRUCTURES. THE HIGHER MEAN OPERATING TEMPERATURES OF THESE COMPOSITES RELATIVE TO METALLIC WALL RESULTS IN R ...

    SBIR Phase I 1990 National Aeronautics and Space Administration
  6. HIGH TEMPERATURE COMPOSITE HOT HYDROGEN CONTROL VALVE DEVELOPMENT

    Amount: $49,834.00

    CERAMIC COMPOSITES PRESENTLY DEMONSTRATE GOOD MECHANICAL PROPERTIES AT TEMPERATURES BELOW 2100 DEG F WITHOUT DEGRADATION AND LOW THERMAL CONDUCTIVITY WITHOUT SACRIFICING THERMAL SHOCK TOLERANCE. THESE ...

    SBIR Phase I 1990 Air ForceDepartment of Defense
  7. ADVANCED SOLIDS DIVERT PROPULSION TECHNOLOGY

    Amount: $49,530.00

    REFRACTORY COMPOSITES, INC. PROPOSES TO UTILIZE CHEMICAL VAPOR INFILTRATION TECHNOLOGY TO PRODUCE GRAPHITE REINFORCED HAFNIUM CARBIDE COMPOSITE NOZZLES FOR EVALUATION AS AN IMPROVED MATERIAL OVER CARB ...

    SBIR Phase I 1990 ArmyDepartment of Defense
  8. VARIABLE POROSITY RADIANT BURNER CONCEPT/DEMONSTRATION

    Amount: $49,459.00

    A VARIABLE POROSITY SILICON CARBIDE CERAMIC FOAM IS DEVELOPED FOR BURNING OF FOSSIL FUELS. THE CONCEPT EMPLOYS BILAYERED RADIANT BURNER OBSERVED SUBSURFACE LOW NOX COMBUSTION RESULTS AND ANALYTICAL MO ...

    SBIR Phase I 1990 Environmental Protection Agency
  9. MIXED HAFNIUM-TANTALUM CARBIDE ROCKET THRUSTER DEVELOPMENT

    Amount: $49,300.00

    RECENT AIR FORCE-FUNDED, ARC-JET MATERIALS TESTING HAS DEMONSTRATED THAT A MIXED HFC-TAC COMPOSITE CERAMIC MATERIAL EXHIBITS THE LOWEST MASS LOSS OF ANY MATERIAL TESTED, INCLUDING HAFNIUM CARBIDE AND ...

    SBIR Phase I 1991 National Aeronautics and Space Administration
  10. LOW COST ROCKET THRUSTERS

    Amount: $60,267.00

    Refractory Composites, Inc. (RCI) proposes to merge innovations in ceramic matrix processing technologies and anvances in fiber weaving technologies to produce dramatic reductions in fabrication costs ...

    SBIR Phase I 1994 Missile Defense AgencyDepartment of Defense

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