VAPORCOR LLC

Company Information

Company Name
VAPORCOR LLC
Address
1044 SE Paiute Way, #101
Bend, OR, 97702
Phone
1 541-678-5215
URL
n/a
DUNS
557258154
Number of Employees
3
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$296,979.00
3
SBIR Phase II
$1,096,578.00
2
Chart code to be here

Award List

  1. Novel Propulsion Using Humphrey Cycle or Other Concepts

    Amount: $98,992.00

    We propose an engine concept, which we call a Cart-Engine, which embodies both a thermodynamic cycle innovation and a mechanical innovation that can achieve exceptional efficiency, low mechanical vibr ...

    SBIR Phase I 2005 Defense Advanced Research Projects AgencyDepartment of Defense
  2. Novel Propulsion Using Humphrey Cycle or Other Concepts

    Amount: $374,571.00

    We propose an engine concept, which we call a Cart-Engine, which embodies both a thermodynamic cycle innovation and a mechanical innovation that can achieve exceptional efficiency, low mechanical vibr ...

    SBIR Phase II 2006 Defense Advanced Research Projects AgencyDepartment of Defense
  3. Very High Altitude Aircraft Propulsion Engines

    Amount: $98,990.00

    Vaporcor has been developing an engine technology that enables a means to implement a Humphrey thermodynamic cycle. In this SBIR, we propose an innovative technical concept and an aggressive business ...

    SBIR Phase I 2007 Defense Advanced Research Projects AgencyDepartment of Defense
  4. Small Engines Designed for High Efficiency, High Power Density and Quiet Operations

    Amount: $98,997.00

    Vaporcor LLC is currently developing a unique engine, (for High Altitude Long Endurance "HALE" aircraft), that has thermodynamic efficiency greater then 40%, is able to burn multiple-fuels, and is qui ...

    SBIR Phase I 2008 Defense Advanced Research Projects AgencyDepartment of Defense
  5. Very High Altitude Aircraft Propulsion Engines

    Amount: $722,007.00

    Vaporcor LLC is developing a very high altitude (~90 kft) aircraft propulsion engine capable of meeting the stability, reliability, and environmental requirements suitable for use on a VHALE aircraft ...

    SBIR Phase II 2009 Defense Advanced Research Projects AgencyDepartment of Defense

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