Ceramic Composites, Inc.

Company Information

Company Name
Ceramic Composites, Inc.
Address
133 Defense Highway, Suite 212
Annapolis, MD, 21401-8907
Phone
1 410-224-3710
URL
n/a
DUNS
783765670
Number of Employees
25
Woman Owned

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$2,861,172.00
38
SBIR Phase II
$4,941,688.00
8
STTR Phase I
$99,988.00
1
Chart code to be here

Award List

  1. CERAMIC MATRIX COMPOSITES FOR MAGNETOHYDRODYNAMIC AIR PREHEATERS

    Amount: $50,000.00

    THIN-WALL CERAMIC COMPOSITE HEAT TRANSFER MATERIALS WITH SUITABLE CORROSION RESISTANCE IN POTASSIUM SEED-LADEN COAL COMBUSTION PRODUCTS ARE POTENTIALLY THE MOST EFFECTIVE METHOD TO PREHEAT THE COMBUST ...

    SBIR Phase I 1992 Department of Energy
  2. Advanced Low Cost Space Radiator

    Amount: $76,772.00

    Space based platforms require substantial on-board power systems with a need for waste heat rejection. Prior work performed on such programs as SUPER has led to the design of carbon/carbon radiators w ...

    SBIR Phase I 1992 Missile Defense AgencyDepartment of Defense
  3. CERAMIC COMPOSITE COMBUSTOR CANS FOR EXPENDABLE TURBINE ENGINES

    Amount: $375,000.00

    A microwave-assisted chemical vapor infiltration (CVI) process is proposed as a low cost method for fabrication of ceramic composite components for expendable turbine engines. In Phase I, optimum proc ...

    SBIR Phase II 1994 Air ForceDepartment of Defense
  4. OXIDE BASED CERAMIC COMPOSTIE HOT GAS FILTER DEVELOPMENT

    Amount: $74,715.00

    HOT GAS PARTICULATE FILTRATION IS CRITICAL TO NEARLY EVERY CLEAN COAL ENERGY CONVERSION TECHNOLOGY. TO DATE, CERAMIC FILTERS HAVE EXHIBITED LIMITED LIFE AND RELIABILITY BECAUSE OF THERMAL SHOCK, THERM ...

    SBIR Phase I 1993 Department of Energy
  5. COMBINED CYCLE ENGINE VARIABLE AREA NOZZLE DEVELOPMENT

    Amount: $74,920.00

    High speed combined cycle propulsion systems have several subsystems in common including the need for a method through which the exhaust nozzle area can be varied to meet the range of altitudes and ve ...

    SBIR Phase I 1993 Air ForceDepartment of Defense
  6. Oxidation Resistant, Hafnium-Carbide-Tantalum-Carbide Rocket Thrusters for High Performance Propellants

    Amount: $69,746.00

    An innovative approach for producing dense adherent, protective oxides for radiatively-cooled C/HfC-TaC ceramic matrix composite (CMC) rocket thrusters capable of handling a broad spectrum of higher p ...

    SBIR Phase I 1994 National Aeronautics and Space Administration
  7. OXIDATION RESISTANT HFC-TAC ROCKET THRUSTER

    Amount: $59,201.00

    A pulsed microwave power, pulsed pressure method that is capable of uniformly and rapidly densifying thick CMC parts to density levels of 95% or greater is proposed. A systematic approach for independ ...

    SBIR Phase I 1994 Missile Defense AgencyDepartment of Defense
  8. TOUGHENED LOW PERMEABILITY C-SIC ROCKET THRUSTER

    Amount: $54,094.00

    Ceramin Composites is please to propose an innovative ceramic composite sheath-monolithic ceramic concept that offers the potential for a tough, low permeability rocket thruster. A previous Phase I SB ...

    SBIR Phase I 1994 Missile Defense AgencyDepartment of Defense
  9. Fiber Reinforced Lightweight Silicon Carbide Mirrors And Telescope

    Amount: $85,693.00

    CCI WILL INVESTIGATE NOVEL CHEMICAL VAPOR INFILTRATION (CVI) PROCESSING TECHNIQUES TO DEMONSTRATE A COMPOSITE MATERIAL CERAMIC (CMC) FABRICATION PROCESS FOR SILICON CARBIDE (SIC) MIRRORS AND OPTICAL C ...

    SBIR Phase I 1994 Missile Defense AgencyDepartment of Defense
  10. Codeposition of Refractory Ir-Al Alloys

    Amount: $59,815.00

    The materials used in current thruster technology meet the performance parameters and environmental constraints needed for missile and space defense with difficulty at best and even then only with a h ...

    SBIR Phase I 1996 Missile Defense AgencyDepartment of Defense

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