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ULTRAMET

Company Information
Address
12173 MONTAGUE ST
PACOIMA, CA 91331-2210
United States


http://www.ultramet.com

Information

UEI: N8ZRMWX85NZ6

# of Employees: 57


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: No

Woman Owned: No



Award Charts




Award Listing

  1. Monopropellant Cubesat Propulsion System

    Amount: $150,000.00

    ABSTRACT: In recent work for the Air Force, Ultramet demonstrated nearly one thousand restarts with repeatable pulse performance and steady-state burn characteristics using AF-M315E monopropellant an ...

    SBIRPhase I2015Department of Defense Air Force
  2. High Heat Flux Block Ablator-in-Honeycomb Heat Shield Using Ablator/Aerogel-Filled Foam, Phase II

    Amount: $750,000.00

    Ultramet and ARA Ablatives Laboratory previously developed and demonstrated foam-reinforced carbon/phenolic ablators that offer substantially increased high heat flux performance and reduced weight re ...

    SBIRPhase II2015National Aeronautics and Space Administration
  3. Laser-Directed CVD 3D Printing System for Refractory Metal Propulsion Hardware, Phase II

    Amount: $900,000.00

    In this work, Ultramet is developing a three-dimensional (3D) laser-directed chemical vapor deposition (CVD) additive manufacturing system to build free-form refractory metal components for liquid roc ...

    SBIRPhase II2015National Aeronautics and Space Administration
  4. Green Monopropellant Secondary Payload Propulsion System

    Amount: $125,000.00

    In recent work for the Air Force, Ultramet demonstrated nearly one thousand restarts with repeatable pulse performance and steady-state burn characteristics using AF-M315E monopropellant and a novel i ...

    SBIRPhase I2015National Aeronautics and Space Administration
  5. Parahydrogen-Orthohydrogen Catalytic Conversion for Cryogenic Propellant Passive Heat Shielding

    Amount: $125,000.00

    The Hydrogen Properties for Energy Research (HYPER) laboratory at Washington State University (WSU) recently demonstrated a Cryocatalysis Hydrogen Experiment Facility (CHEF) to characterize parahydrog ...

    SBIRPhase I2015National Aeronautics and Space Administration
  6. Rapid Manufacturing of Durable, Cost-Effective Ceramic Matrix Composites for High Temperature Structures

    Amount: $125,000.00

    Hypersonic vehicles require durable and cost-effective hot structures that do not impose weight penalties such as those associated with the use of non-structural thermal protection systems. In previou ...

    SBIRPhase I2015National Aeronautics and Space Administration
  7. Low-Cost, Lightweight Transpiration-Cooled LOX/CH4 Engine

    Amount: $125,000.00

    The specific impulse of a rocket engine increases as the chamber pressure increases, but so does the heat flux to the chamber wall. Ultimately, this defines the maximum operating pressure for the engi ...

    SBIRPhase I2015National Aeronautics and Space Administration
  8. Low-Cost, Lightweight, High-Performance CMC Combustion Chamber for HAN-Based Monopropellant Engines

    Amount: $125,000.00

    Non-toxic storable liquid propulsion systems are of great interest for use in future exploration missions. Efficient propulsive performance and long-duration storage attributes have made the use of hy ...

    SBIRPhase I2015National Aeronautics and Space Administration
  9. Fabrication and Testing of Nuclear-Thermal Propulsion Ground Test Hardware, Phase II

    Amount: $750,000.00

    Efficient nuclear-thermal propulsion (NTP) requires heating a low molecular weight gas, typically hydrogen, to high temperature and expelling it through a nozzle. The higher the temperature and pressu ...

    SBIRPhase II2015National Aeronautics and Space Administration
  10. High-Performance Cellular Lithium Titanate Solid Breeder Material with Enhanced Tritium Release

    Amount: $150,000.00

    Solid breeder materials that have been considered in the past are all lithium-based ceramics, including lithium oxide, silicate, titanate, and zirconate, in pebble-bed configurations to enhance tritiu ...

    SBIRPhase I2015Department of Energy
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