Electric Propulsion Laboratory Inc

Company Information

Company Name
Electric Propulsion Laboratory Inc
Address
1040 Synthes Ave
Monument, CO, 80132
Phone
1 719-481-4411
URL
n/a
DUNS
n/a
Number of Employees
n/a
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$1,163,982.00
16
SBIR Phase II
$3,791,837.00
8

Award List

  1. HIGH POWER ELECTRIC PROPULSION CONCEPTS ASSESSMENT FOR ENHANCED MISSION CAPABILITY

    Amount: $150,000.00

    HIGH SPECIFIC IMPULSE ELECTRIC PROPULSION CONCEPTS WILL BE INVESTIGATED FOR OPERATION IN THE 0.1-5 MW POWER RANGE TO SUBSTANTIALLY REDUCE PROPELLANT MASS REQUIREMENTS AND SUBSEQUENT COST, OVER CHEMICA ...

    SBIR Phase II 1988 Missile Defense AgencyDepartment of Defense
  2. PLASMA CONTAINMENT SCHEME FOR HIGH THRUST DENSITY ION ENGINES

    Amount: $499,000.00

    PRESENT ION ENGINE TECHNOLOGY IS LIMITED IN ENGINE THRUST DENSITY AND EFFICIENCY BY ENERGY EXPENSIVE PLASMA PRODUCTION PROCESSES AND BY ION ACCELERATOR SYSTEM DESIGNS WHICH LIMIT THE ATTAINABLE BEAM C ...

    SBIR Phase II 1988 Missile Defense AgencyDepartment of Defense
  3. ARCJET SELF-GETTER PUMPING

    Amount: $49,816.00

    A NOVEL, HIGH THROUGHPUT, TITANIUM GETTER VACUUM PUMPING CONCEPT THAT UTILIZES THE KINETIC ENERGY IN THE PLASMA JET EMANATING FROM AN ARCJET ENGINE AS THE GETTER PUMPING POWER SOURCE IS PROPOSED. CALC ...

    SBIR Phase I 1990 Air ForceDepartment of Defense
  4. AN ELECTROSTATIC PLASMA ACCELERATOR PROPULSION SYSTEM FOR SMALL SATELLITES

    Amount: $49,993.00

    A SIMPLE, HIGH SPECIFIC IMPULSE ELECTRIC PROPULSION THRUSTER IS PROPOSED FOR APPLICATION TO SMALL SATELLITES. THIS THRUSTER USES AN ELECTROSTATIC PLASMA ACCELERATION (EPA) PRINCIPLE TO ACHIEVE PROJECT ...

    SBIR Phase I 1990 Defense Advanced Research Projects AgencyDepartment of Defense
  5. HIGH PERFORMANCE, VARIABLE POWER AMMONIA ARCJET

    Amount: $398,479.00

    AN AGGRESSIVE ARCJET CONFIGURATION OPTIMIZATION PROGRAM IS PROPOSED TO DESIGN A HIGH PERFORMANCE, VARIABLE POWER AMMONIA ARCJET. A NOVEL TEST BED ARCJET AND MODULAR NOZZLE DESIGN APPROACH IS PROPOSED ...

    SBIR Phase II 1992 Air ForceDepartment of Defense
  6. LOW FLOW ARC HEAD VACUUM WELDING

    Amount: $207,673.00

    ON-ORBIT WELDING FOR EITHER ASSEMBLY OR REPAIR OF FUTURE SPACE STATIONS AND PLATFORMS WILL REQUIRE NOVEL APPROACHES TO THE DESIGN OF THE ARC-TYPE WELDING HEADS, TO ENSURE THAT THIS VERY SUCCESSFUL FOR ...

    SBIR Phase II 1992 National Aeronautics and Space Administration
  7. High Performance Insulators for Electric Propulsion Engines

    Amount: $73,738.00

    New technology, high performance insulators are critical to improved electric propulsion engine operation and lifetime. Little work has been done on investigating the advances in dielectric materials ...

    SBIR Phase I 1993 Air ForceDepartment of Defense
  8. Methane Arcjet Sooting Evaluation and Control

    Amount: $75,000.00

    Methane propellant has the potential for achieving arcjet performance levels close to that of pure hydrogen. However, methane has a cryogenic storage density six times that of hydrogen, and a 100 C hi ...

    SBIR Phase I 1993 Air ForceDepartment of Defense
  9. New Technology Resistojet

    Amount: $98,211.00

    A new technology resistojet is proposed as the answer to significantly increasing the proposed as the answer to significantly increasing the propulsion, and thereby mission capability, of future small ...

    SBIR Phase I 1996 Air ForceDepartment of Defense
  10. Charging Hazard Event Controller (CHEC) System

    Amount: $96,945.00

    N/A

    SBIR Phase I 1999 Air ForceDepartment of Defense

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