SPIRITECH Advanced Products, Inc.

Company Information

Company Name
SPIRITECH Advanced Products, Inc.
Address
731 N US Highway 1
Suite 1
Tequesta, FL, -
Phone
561-741-3441
URL
http://www.spiritech.cc
DUNS
17391348
Number of Employees
11
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$1,369,744.00
14
SBIR Phase II
$2,999,549.00
4
Chart code to be here

Award List

  1. Rotating Chamber Pulse Detonation Engine

    Amount: $69,949.00

    Pulse detonation engines hold promise to increase performance of air-breathing propulsion systems by taking advantage of the increase in cycle efficiency due to the constant-volume heat addition chara ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  2. Improving Off-Design Nozzle Performance Using Fluidic Injection

    Amount: $69,996.00

    Use of fluidic injection of high-pressure air is proposed to improve nozzle performance and reduce the off-axis component of thrust at off-design flight conditions, generally at low Mach number and lo ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  3. Flow Test for Rotating Chamber Pulse Detonation Engine

    Amount: $69,956.00

    Pulse detonation engines hold promise to increase performance of air-breathing propulsion systems by taking advantage of the increase in cycle efficiency due to the constant-volume heat addition chara ...

    SBIR Phase I 2003 National Aeronautics and Space Administration
  4. Fluidic Nozzle to Improve Transonic Performance of Hypersonic Vehicle

    Amount: $99,988.00

    Use of fluidic injection of high-pressure air is proposed to improve a hypersonic vehicle's installed nozzle performance and eliminate undesirable pitching moments at off-design, transonic flight cond ...

    SBIR Phase I 2004 Air ForceDepartment of Defense
  5. Confined Recirculation Combustion Afterburner

    Amount: $749,694.00

    The future of manned and unmanned vehicles requires significant improvements in engine thrust-to-weight ratio, efficiency, length, and cost. These improvements may be realized in the afterburner for s ...

    SBIR Phase II 2005 Air ForceDepartment of Defense
  6. Confined Recirculation Combustion Afterburner

    Amount: $99,975.00

    The future of manned and unmanned vehicles requires significant improvements in engine thrust-to-weight ratio, efficiency, length, and cost. These improvements may be realized in the afterburner for s ...

    SBIR Phase I 2004 Air ForceDepartment of Defense
  7. CMC Combustor Liner

    Amount: $99,975.00

    Ceramic Matrix Composites (CMC's) offer substantial weight reductions over metallic components, increasing vehicle range and/or payload, as well as reducing cooling flow requirements, thereby increasi ...

    SBIR Phase I 2005 Air ForceDepartment of Defense
  8. CMC Combustor Liner

    Amount: $749,940.00

    The future of manned and unmanned vehicles requires significant improvements in engine thrust-to-weight ratio, efficiency, and engine operating temperatures. One area where these improvements may be ...

    SBIR Phase II 2006 Air ForceDepartment of Defense
  9. Scramjet/Ramjet Heat Exchanger Analysis Tool

    Amount: $99,989.00

    A ramjet/scramjet heat exchanger design and optimization tool is proposed for rapid analyses of complex thermal cooling systems. In the emerging field of high-speed aerospace, it is necessary that rap ...

    SBIR Phase I 2005 Air ForceDepartment of Defense
  10. Scramjet/Ramjet Heat Exchanger Analysis Tool

    Amount: $749,943.00

    A Scramjet/Ramjet Heat Exchanger Analysis Tool (SRHEAT(TM)) is proposed for rapid design and optimization of complex thermal cooling systems. The basic SRHEAT(TM) code was developed under the Phase I ...

    SBIR Phase II 2006 Air ForceDepartment of Defense

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