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ZONA TECHNOLOGY INC

Company Information
Address
9489 E IRONWOOD SQUARE DR
SCOTTSDALE, AZ 85258-4578
United States


http://www.zonatech.com

Information

UEI: LYMKH9UK64J7

# of Employees: 7


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: Yes

Woman Owned: No



Award Charts




Award Listing

  1. N/A

    Amount: $597,292.00

    N/A

    SBIRPhase II1999National Aeronautics and Space Administration
  2. Adaptive Reconfigurable Control Based on a Reduced Order System Identification for Flutter and Aeroservoelastic Instability Suppression

    Amount: $69,779.00

    Not Available Axial and divert motors and nozzles require complex shapes which are light weight, strong and shock resistant at high temperatures. Carbon-carbon (C-C) is an ideal material for this app ...

    SBIRPhase I1999Department of Defense Navy
  3. Formulation and Application of a Stochastic Fatigue Damage Accumulation Model for the Acoustic Response of Buckled Composite Panels

    Amount: $84,557.00

    N/A

    SBIRPhase I1999Department of Defense Air Force
  4. N/A

    Amount: $562,068.00

    N/A

    SBIRPhase II1999Department of Defense Air Force
  5. Nonlinear Reduced Order Modeling of Limit Cycle Oscillations of Aircraft Wiings

    Amount: $99,893.00

    N/A

    STTRPhase I1999Department of Defense Air Force
  6. A Variable Stiffness Spar (VSS) Approach for Aircraft Maneuver Enhancement

    Amount: $99,812.00

    An innovative variable stiffness spar (VSS) approach is proposed for the enhancement of aircraft roll performance. F/A-18 pre-roll-modification aircraft (F/A-18 PRM) is selected as the baseline aircr ...

    SBIRPhase I1998Department of Defense Air Force
  7. CFD/CSD Interfacing via an Innovative Structural Boundary Element Method

    Amount: $68,337.00

    N/A

    SBIRPhase I1998National Aeronautics and Space Administration
  8. Aeroelastic/Aeroservoelastic Tailoring for Hinge Moment Minimization of Missile Fins

    Amount: $69,522.00

    The primary objective of the present SBIR proposal is to develop a new design methodology and applying it to demonstrate the feasibility of rendering minimized missile fin hinge moment covering all ...

    SBIRPhase I1997Department of Defense Navy
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