TechLand Research, Inc.

Company Information
Address 28895 Lorain Road
Suite 201
North Olmsted, OH, -


Information

DUNS: 967185414

# of Employees: 5


Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N



Award Charts




Award Listing

  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 ...

    SBIRPhase I2015Department 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 ...

    SBIRPhase I2012Department 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 ...

    SBIRPhase I2005National 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 ...

    SBIRPhase II2003Air 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 ...

    SBIRPhase I2003Air 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 ...

    SBIRPhase I2002National 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 ...

    SBIRPhase II2001National 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 ...

    SBIRPhase I2001National Aeronautics and Space Administration
  9. N/A

    Amount: $69,918.00

    N/A

    SBIRPhase I2000National Aeronautics and Space Administration
  10. Mixed-Compression Inlet for Supersonic Cruise with High Performance and Operability

    Amount: $69,948.00

    N/A

    SBIRPhase I1998National Aeronautics and Space Administration

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