TechLand Research, Inc.

Company Information

Company Name
TechLand Research, Inc.
Address
28895 Lorain Road
Suite 201
North Olmsted, OH, -
Phone
1 440-716-9077
URL
n/a
DUNS
967185414
Number of Employees
5
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N

Award Totals

PROGRAM/PHASE
AWARD AMOUNT ($)
NUMBER OF AWARDS
SBIR Phase I
$528,433.00
8
SBIR Phase II
$1,836,690.00
3

Award List

  1. N/A

    Amount: $69,918.00

    N/A

    SBIR Phase I 2000 National Aeronautics and Space Administration
  2. Flight Testing of a New Design Concept for Axisymmetric Inlets

    Amount: $599,974.00

    This proposal identifies a flight test program on the F-15B at NASA Dryden to obtain off-design performance of high-speed inlets that incorporate a unique variable geometry system. The proposed effort ...

    SBIR Phase II 2001 National Aeronautics and Space Administration
  3. Flight Testing of a New Design Concept for Axisymmetric Inlets

    Amount: $0.00

    This proposal identifies a flight test program on the F-15B at NASA Dryden to obtain off-design performance of high-speed inlets that incorporate a unique variable geometry system. The proposed effort ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  4. High-Performance, Low-Sonic-Boom Supersonic Cruise Inlet

    Amount: $69,653.00

    This proposal describes a research study to define a high-speed inlet model for flight-testing on the F-15B at NASA Dryden. The objectives of the flight test program are to obtain off-design performan ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  5. Airflow Controller and Isolator for Pulse Detonation Engines

    Amount: $644,022.00

    The development of a revolutionary airflow controller and isolator for application with a high-speed inlet and a pulse detonation engine (PDE) is proposed. This innovation has the potential of provid ...

    SBIR Phase II 2003 Air ForceDepartment of Defense
  6. Airflow Controller and Isolator for Pulse Detonation Engines

    Amount: $99,129.00

    A revolutionary airflow controller and isolator for application with a high-speed inlet and a pulse detonation engine (PDE) is proposed. This innovation has the potential of providing a solution to t ...

    SBIR Phase I 2003 Air ForceDepartment of Defense
  7. Mode Transition Variable Geometry for High Speed Inlets for Hypersonic Aircraft

    Amount: $69,915.00

    Hypersonic propulsion research has been a focus of the NASA aeronautics program for years. Previous high-speed cruise and space access programs have examined the problems of inlet design for hybrid s ...

    SBIR Phase I 2005 National Aeronautics and Space Administration
  8. Mixed-Compression Inlet for Supersonic Cruise with High Performance and Operability

    Amount: $69,948.00

    N/A

    SBIR Phase I 1998 National Aeronautics and Space Administration
  9. Design Of A High Performance External-Compression Inlet For Cruise At Mach 2.4

    Amount: $69,902.00

    N/A

    SBIR Phase I 1997 National Aeronautics and Space Administration
  10. Design Of A High Performance External-Compression Inlet For Cruise At Mach 2.4

    Amount: $592,694.00

    N/A

    SBIR Phase II 1998 National Aeronautics and Space Administration

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