TechLand Research, Inc.

Basic Information

28895 Lorain Road
Suite 201
North Olmsted, OH, -

Company Profile

n/a

Additional Details

Field Value
DUNS: 967185414
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 5


  1. Innovative Methods for Parametric Bleed Pattern Variation in Wind Tunnel Models

    Amount: $149,862.00

    ABSTRACT: A research effort to investigate innovative approaches to rapid and simple variation of bleed patterns in high-speed inlet wind tunnel models is proposed. Variation of inlet bleed patterns ...

    SBIR Phase I 2014 Department of Defense Air Force
  2. Design of a Highly Compact Supersonic Cruise Missile (SSCM) Inlet

    Amount: $79,968.00

    The objective of the proposed effort is to demonstrate the feasibility of designing a Mach 2.5 inlet for a high-speed cruise missile. This inlet must provide the proper airflow to a turbojet engine fo ...

    SBIR Phase I 2012 Department of Defense Navy
  3. 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
  4. 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 Force Department of Defense
  5. 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 Force Department of Defense
  6. 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
  7. 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
  8. 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
  9. N/A

    Amount: $69,918.00

    N/A

    SBIR Phase I 2000 National Aeronautics and Space Administration
  10. 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

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