Ultramet

Company Information

Company Name
Ultramet
Address
12173 Montague Street
Pacoima, CA, 91331-2210
Phone
1 818-899-0236
URL
http://www.ultramet.com
DUNS
95
Number of Employees
70
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$16,659,149.00
213
SBIR Phase II
$54,320,991.00
92
STTR Phase I
$300,000.00
4
STTR Phase II
$990,609.00
2

Award List

  1. Low-Cost Refractory Metal-Lined Graphite Components for Advanced SDACS

    Amount: $99,778.00

    Rhenium hot gas path components are used extensively in the solid divert and attitude control system (SDACS) of the MDA/Navy Standard Missile-3 Aegis LEAP Interceptor missile defense program, on which ...

    SBIR Phase I 2010 Missile Defense AgencyDepartment of Defense
  2. Lightweight Hybrid Ablator Incorporating Aerogel-Filled Open-Cell Foam Structural Insulator, Phase II

    Amount: $600,000.00

    In previous work for NASA and DoD, Ultramet developed lightweight open-cell foam insulators composed of a carbon or ceramic structural foam skeleton filled with a high temperature nanoscale aerogel in ...

    SBIR Phase II 2010 National Aeronautics and Space Administration
  3. Aerogel-Filled Foam Core Insulation for Cryogenic Propellant Storage

    Amount: $100,000.00

    Current cryogenic insulation materials suffer from various drawbacks including high cost and weight, lack of structural or load-bearing capability, fabrication complexity, and property anisotropy. A n ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  4. Alumina Fiber-Reinforced 9310 Steel Metal Matrix Composite for Rotorcraft Drive System Components

    Amount: $100,000.00

    AISI 9310 nickel-chromium-molybdenum alloy steel is used extensively in military helicopter rotor shafts and gears. This reliable alloy provides excellent fatigue life combined with high hardness, ela ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  5. Low-Cost, High-Performance Combustion Chamber for LOX/CH4 Propulsion

    Amount: $100,000.00

    Ultramet will design and fabricate a lightweight, high temperature 5-lbf combustion chamber for use with cryogenic liquid oxygen/methane (LOX/CH4) propellant that will deliver a specific impulse of ~3 ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  6. Low-Cost, Ultrahigh Temperature Zero-Erosion Ceramic Matrix Composite for SM-3 TDACS Divert Valve Pintles, Phase II

    Amount: $999,877.00

    Future performance goals for ballistic missile defense systems necessitate the development of zero-erosion throat materials for boost and tactical solid rocket motors. Increasing demands imposed by ad ...

    SBIR Phase II 2010 Missile Defense AgencyDepartment of Defense
  7. Foam-Based Ignition System for Non-Toxic Propellants, Phase II

    Amount: $723,303.00

    Hydroxylammonium nitrate (HAN)-based monopropellants promise many improvements over monopropellant hydrazine and bipropellant nitrogen tetroxide/monomethyl hydrazine (NTO/MMH). But before HAN-based mo ...

    SBIR Phase II 2010 Department of Defense
  8. High-Hardness Lightweight Body Armor

    Amount: $70,000.00

    Current Enhanced Small Arms Protective Insert (E-SAPI) plates are made from hot-pressed boron carbide (B4C), which offers a favorable combination of high hardness and light weight. As threats continue ...

    SBIR Phase I 2010 NavyDepartment of Defense
  9. IN ORDER TO ACHIEVE INCREASED EFFICIENCY, LIFE, AND PERFORMANCE, ROCKET ENGINES REQUIRE OPERATION AT HIGHER AND HIGHER TEMPERATURES.

    Amount: $49,427.00

    IN ORDER TO ACHIEVE INCREASED EFFICIENCY, LIFE, AND PERFORMANCE, ROCKET ENGINES REQUIRE OPERATION AT HIGHER AND HIGHER TEMPERATURES. IN ORDER TO OBTAIN SUFFICIENT STRENGTH AT THESE TEMPERATURES, THE R ...

    SBIR Phase I 1983 Air ForceDepartment of Defense
  10. HIGH TEMPERATURE OXIDATION RESISTANT COATINGS

    Amount: $499,200.00

    IN ORDER TO ACHIEVE INCREASED EFFICIENCY, LIFE, AND PERFORMANCE, ROCKET ENGINES REQUIRE OPERATION AT HIGHER AND HIGHER TEMPERATURES. IN ORDER TO OBTAIN SUFFICIENT STRENGTH AT THESE TEMPERATURES, THE R ...

    SBIR Phase II 1984 Air ForceDepartment of Defense

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