ZONA TECHNOLOGY INC

Scottsdale, AZ · Aerospace · Acquired by Siemens (2022)

CFD-based aeroelastic and aeroservoelastic analysis software (ZAERO++)

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Updated Oct 23, 2026 · zonatech.com

Sector: Aerospace
Headquarters: Scottsdale, AZ
Total capital: $24.6M

Federal grants: $1.9M; 5 awards · 2014–2021; Rank in peer group#5 of 44
Private capital raised: None on recordNo Form D filings on SEC EDGAR. Some raises are not filed.
Federal contracts: $22.7M; 105 awards · Defense, NASA; Rank in Aerospace#140 of 1335
Granted patents: None on recordNo USPTO grants. Applications publish after 18 months.

Capital timeline

Latest events

Apr 2024Federal contractDefense · Zaero Renewal$17K
Jun 2023Federal contractDefense · Zaero III$17K
May 2022Federal contractDefense · Zaero III Software Renewal$17K
Jul 2021Federal grantNASA · Phase II · Generation of CFD-Based Structurally Independent Aerodynamic Influence Coefficient Matrix$750K
Mar 2021Federal contractDefense · Zaero III Sw Renewal Of Existing Licenses$25K
Sep 2020Federal contractDefense · Bayesian-based Probabilistic Limit Cycle Oscillation Prediction Of Aircraft With Stores$750K
Aug 2020Federal contractNASA · Generation Of Cfd-based Structurally Independent Aerodynamic Influence Coefficient Matrix$125K

Show 102 earlier federal awards

May 2020Federal contractNASA · Zona Technology License Renewal$32K
Mar 2020Federal contractDefense · Zaero III Softwarerenewal$25K
Aug 2019Federal contractNASA · The Overall Technical Objective Of The Phase II Effort Is To Make Overfun As A Fully Multi-functional Aeroelastic Software System That Can Establish Either The Discrete Time State-space Plant Model Or The Frequency-domain Aeroelastic Equation Of Motion With Three Embedded Unsteady Aerodynamic Sub-systems; Due To The Structural Deformation, The Control Surface Deflection And The Discrete Gust Excitation, Respectively. All Three Unsteady Aerodynamic Sub-systems Can Be Obtained By Applying The Exte$750K
Jul 2019Federal contractNASA · Cfd-based Reduced Order Modeling (rom) Has Been An Active Research Area, As They Can Be Used Directly With Common Linear Flutter Analysis Tools. Among Them, Linearized Reduced-order Modeling Approaches Rely On Linearization Of The Nonlinear Unsteady Aerodynamic Flow Equations, Assuming That The Amplitude Of The Unsteady Motion Is Limited To Small Perturbations About The Nonlinear Steady-state Flow Condition. Various Approaches Of Linearized Roms, Such As Auto-regressive-moving-average (arma), Fi$124K
May 2019Federal contractDefense · Bayesian-based Probabilistic Limit Cycle Oscillation Prediction Of Aircraft With Stores$150K
Apr 2019Federal contractNASA · Ot This Is A Purchase Order For Zona Technology Software Renewal. Quote Number QNASA21519 A, B And C, Dated 02/15/2019.$69K
Mar 2019Federal contractDefense · FUN3D-BASED Sensitivity Analysis For Fourth Generation Fighter In Chaotic Flows$750K
Jan 2019Federal contractDefense · Zaero Software License Renewal$17K
Dec 2018Federal contractDefense · Non Acat, Zona Tech, Afit, Licenses$8K
Sep 2018Federal contractDefense · Uniformed Aeroelsatic Rom$747K
May 2018Federal contractNASA · Ot: 2 - Zaero III 1ST&2ND Token, 1 - Ase Option 1ST Token, 1 - Trim Option 1ST Token, 1 - Zaero III 3RD Token, 1 - Zaero III 4TH Token, 1 - Ase Option 2ND Token, 1 - Trim Option 2ND Token, 1 - Dynamic Loads Option 1ST Token, 1 - Gust Option 1ST Token, 1 - Whirl Flutter Option 1ST Token, 1 - Zaero III 5TH Token, 1 - Ase Option 3RD Token And 1 - Trim Option 3RD Token$72K
Feb 2018Federal contractDefense · Zaero Software License Renewal$17K
Aug 2017Federal contractNASA · Igf::ot::igfcreate A Crate And Meet Shipment Instructions For Shipment Of The Model And To Physical Ship The Model With Insurance And Meet The Delivery Instructions.$10K
Aug 2017Federal contractDefense · Igf::ot::igf Adjoint Optimization For Elastic Tandem Airfoils$150K
Jul 2017Federal contractDefense · Zaero III$23K
Jun 2017Federal contractDefense · Non-acat, Afit, Zona Technology Software, Base Year With Options$8K
Jun 2017Federal grantDefense · Phase I · Multiple Level Reduced Order Modeling for Ship Airwake Modeling and Simulation$125K
May 2017Federal contractNASA · Igf::ot::igf Zona Technologies Zaero III Renewal$72K
Apr 2017Federal contractNASA · Igf::ot::igf The Nonlinear Dynamic Flight Simulation (nl-dfs) System Will Be Developed In The Phase II Project By Combining The Classical Nonlinear Rigid-body Flight Dynamics Model With An Add-on Nonlinear Aeroelastic Solver To Compute The Airframe Response Due To Pilot Input Command And To Identify The Key Aeroelastic Coupling Mechanisms Between The Structural Dynamics And Unsteady Aerodynamics With Classic Rigid-body Dynamics. The Nonlinear Aeroelastic Solver Solves The Aeroelastic Equation O$735K
Mar 2017Federal contractDefense · Zaero Software$17K
Aug 2016Federal grantDefense · Phase I · RANS-Based Stick-to-Stress Dynamic Flight Simulation for Aircraft Life Prediction$150K
Aug 2016Federal contractDefense · Non-acat, Afit, Zona Software$8K
Jul 2016Federal contractDefense · Igf::ot::igf (STTR Phase II) Development Of An Efficient Flutter And Limit Cycle Oscillation Predictive Tool$749K
Jun 2016Federal contractNASA · Igf::ot::igf The Overall Technical Objective Of The Phase I Effort Is To Develop A Nonlinear Aeroelastic Solver Utilizing The FUN3D Generated Nonlinear Aerodynamic Reduced Order Model (rom). Two Types Of Aerodynamic Reduced Order Models Will Be Developed; The First Is The Neural Network Nonlinear Rom That Can Provide The Aerodynamic Feedback Forces Due To Structural Deformation And The Second Is A Nonlinear Volterra-kernels-based Gust Rom That Provides The Aerodynamic Forces Due To Gust Excitat$125K
May 2016Federal contractNASA · Zaeroiii, Ase Option, And Trim Option Software Renewals$72K
May 2016Federal contractDefense · Non-acat, Afrl, Zona Zaero Software Support$44K
Jan 2016Federal contractDefense · Zaero III$17K
Jul 2015Federal grantDefense · Phase II · Stick-to-Stress Dynamic Flight Simulation for Predicting Fatigue Life and Scheduling Inspections of Aircraft$750K
May 2015Federal contractNASA · Zaero III 5TH Token; Ase Option 2ND Token; Trim Option 3RD Token Renewals$15K
Apr 2015Federal contractNASA · Igf::ot::igf In Phase I, A Prototypical FUN3D-BASED Zona Euler Unsteady Solver (funzeus) Was Developed To Generate The Generalized Aerodynamic Forces (gafs) Due To Structural Modes, Control Surface Kinematic Modes, And Gust Excitation Using A Frequency-domain Linearized Unstructured Euler Solver Based On The Navier-stokes Solution Of FUN3D As The Steady Background Flow. These Gafs Can Lead To A State-space Equation Representing The Plant Model For Rapid Aeroelastic And Aeroservoelastic (ase) Des$750K
Apr 2015Federal contractNASA · Zaero Software Maintenance Renewal$54K
Apr 2015Federal contractDefense · Non Acat, Afrl/rqv Zona Zaero Software$44K
Dec 2014Federal contractDefense · Zaero Option III$24K
Oct 2014Federal grantDefense · Phase I · Development of an Efficient Flutter and Limit Cycle Oscillation Predictive Tool$150K
Sep 2014Federal contractDefense · Igf::ot::igf SBIR II Zona Technologies$747K
Sep 2014Federal contractDefense · Non-acat, Afrl/rqoc, Zaero Software$44K
Jul 2014Federal contractNASA · Zaero Option III; Ase Option; And Trim Option$11K
Jun 2014Federal contractNASA · Igf::ot::igf The Overall Technical Objective Of This Multi-phase Project Is To Develop And Validate A So-called 'aaw-process' That Consists Of (i) The Active Aeroelastic Wing (aaw) Technology Of Employing Multiple Control Surfaces In Tandem For Achieving Loads Alleviation And Drag Minimization Using The Over-determined Trim Capability Of Zona Euler Unsteady Solver (zeus), And (II) The Aeroelastic Tailoring Technique For Optimum Stiffness Distribution And Weight Minimization While Satisfying Str$750K
Jun 2014Federal contractNASA · Igf::ot::igf The Overall Objective Of This Phase I Project Is To Develop A Nonlinear Trim Module In FUN3D For Enabling The Determined And Over-determined Trim Analyses To Be Performed By FUN3D With Static Aeroelastic Effects. Based On An Optimization Formulation, The Over-determined Trim Analysis Can Determine The Optimum Control Surface Scheduling Of Multiple Control Surfaces To Achieve The Best Aerodynamic Efficiency Of The Aircraft Using The High-fidelity Navier-stokes (n-s) Solver In FUN3D.$125K
Jun 2014Federal contractNASA · Igf::ot::igf The Overall Objective Of This Phase I Project Is To Develop A Hybrid Approach In FUN3D, Referred Herein To As The Linearized FUN3D, For Rapid Aeroelastic And Aeroservoelastic (ase) Design And Analysis. The Linearized FUN3D Solves A Linearized Euler Equation With A Transpiration Boundary Condition Using The FUN3D Steady N-s Solution As The Steady Background Flow To Efficiently Generate A Reduced Order Model (rom) In The Form Of The Frequency-domain Generalized Aerodynamic Forces (gaf$125K
May 2014Federal contractDefense · Igf::ot::igf Zona Technology, Inc. SBIR I AF141-066$150K
Apr 2014Federal contractNASA · Zaero Option III, Ase, Trim, Dynamic Loads, And Gust Option Software Licenses$54K
Mar 2014Federal contractDefense · Igf::ot::igf "(STTR Phase II) Sensitivity Analysis Methods For Complex, Multidisciplinary Systems"$747K
Feb 2014Federal contractDefense · Zaero Option III$17K
Sep 2013Federal contractDefense · Non-acat, Afrl/rqoc, Zaero Software Renewal$44K
Aug 2013Federal contractDefense · Non-acat, Afit, Zareo&zeus Software Renewal$24K
Jun 2013Federal contractNASA · Igf::ot::igf Zaero License$21K
May 2013Federal contractNASA · Igf::ot::igf The Overall Objective Of This Multi-phase Project Is To Explore, Develop, Integrate, And Test Several Innovative Structural Design Concepts And New Material Possibilities That Will Fully Leverage The Expertise Of The Zona/boeing Team For Enhancing The Current State-of-the-art Of Aircraft Design. The Technical Objectives Specific To The Phase I Of This Effort Are Threefold. First, A Suitable Anisotropic Composite Material Will Be Identified And Further Studied For Its Suitability To$125K
Mar 2013Federal contractNASA · Licensing Of The Zaero Software System$24K
Feb 2013Federal contractDefense · Igf::ot::igf STTR Phase II - Stick-to-stress Dynamic Flight Simulation For Virtual Flight Test$750K
Jan 2013Federal contractNASA · Igf::ot::igf - During Phase I Of This Effort, Zona Technology, Inc. Significantly Improved The Medium Fidelity Design And Analysis Capability Of Nasa's Mdao Architecture By Successfully Adding Zona Cae Tools Such As Zaero, Zeus, Astros And Zmorph Synergistically Integrated Within A Modelcenter Mdao Framework. In Phase II Of This Effort, Zona Aims To Improve All The Three Tiers Of Nasa's Mdao Architecture As Follows: (1) The Low Fidelity Capability Will Be Enhanced By Incorporating Zonair For Pro$685K
Sep 2012Federal contractDefense · Zaero Option III$17K
Aug 2012Federal contractDefense · Zaero Option III Software$24K
Aug 2012Federal contractDefense · Non-acat, Afit/eny, Zaero And Zeus Software$11K
May 2012Federal contractDefense · Zona Technology, Inc. New Phase I - AF12-1-208$150K
Apr 2012Federal contractNASA · Igf::ot::igf Other Functions Zona Technology Software$24K
Apr 2012Federal contractDefense · Zaero Software$44K
Mar 2012Federal contractDefense · "(STTR Phase 1) Sensitivity Analysis Methods For Complex, Multidisciplinary Systems"$100K
Feb 2012Federal contractNASA · Zona Technology, Inc. Proposes An R&d Effort To Develop A Gust Load Alleviation (gla) Control System Using A Novel Leading Edge Stagnation Point (lesp) Sensor That Has The Nearly Instantaneous Predictive Capability. The Real-time Gust Information From The Sensor Will Enhance The Performance Of The Proposed Gla Control System. The Gla Control Method We Will Adopt Is The Generalized Predictive Control (gpc), Which Consists Of Identification Of The Flexible System Perturbed By Gusts And Minimizatio$125K
Feb 2012Federal contractNASA · In This Effort, Zona Technology, Inc. Aims At Developing An Innovative Multi-fidelity And Multi-disciplinary Optimization (mdo) Sub-framework That Can (i) Effectively Reduce The Number Of Design Variables Without Screening-out Any Of The Variables, (II) Accelerate The Convergence Through A Novel Design Space Evolution Technique, And (III) Enable Rapid Determination Of Design Sensitivities (gradients) For All The Levels Of Fidelity During Aerodynamic Analyses. The Innovative Application Of Proper$125K
Dec 2011Federal contractDefense · (STTR Ph. 1) Stick-to-stress Dynamic Flight Simulation For Virtual Flight Test$100K
Sep 2011Federal contractDefense · Zaero Sw Licenses$44K
Jul 2011Federal contractDefense · Zaero Software System$24K
Jul 2011Federal contractDefense · Zona Zeus Research Software$5K
Jun 2011Federal contractNASA · Zona Technology, Inc. Proposes To Develop An Integrated Flight Dynamics Simulation Capability With Nonlinear Aeroelastic Interactions By Combining A Flight Dynamics Model And An Add-on Nonlinear Aeroelastic Solver In A Simulink Environment. This Nonlinear Aeroelastic Solver Is Generated By Interacting A Nonlinear Structural Reduced Order Model (rom) With A Neural-network-based (nn-based) Aerodynamic Rom And A Gust Rom To Provide The Incremental Aeroelastic Forces And Moments Of A Classical Fligh$600K
Jun 2011Federal contractNASA · Zona Technology, Inc. (zona) Proposes To Develop An On-line Flutter Prediction Tool Using The Parameter Varying Estimation (pve) Methodology, Called The Pve Toolbox, To Ensure The Flight Safety During The Flight Flutter Test And To Prevent The Damage To The Wind Tunnel Hardware From The Structural Failure Of The Flutter Model During Wind Tunnel Flutter Test. This Tool Can Be Applied To Rapidly Identify Parameters, Such As Modal Damping And Frequency From Test Data Measured At Pre-flutter Flight/$600K
May 2011Federal contractNASA · Sap Purchase Requisition: 4200386301 Zaero Software Maintenance Renewal For The Following: Zaero Option III, Ase Option And Trim Option$24K
Feb 2011Federal contractNASA · Zona Proposes A Unified Gas Kinetic Scheme (ugks) To Cover The Full Knudsen Number Range From The Continuum Flow To Free Molecular Flow That Can Simultaneously Exist In The Jet Nozzle Flow Of The Spacecraft. In The Ugks Solver, The Bgk Model Of Boltzmann Equation Is Solved Directly With Finite Volume Method Based On The Discrete Ordinate Method (dom). In The Ugks Computation The Convective Terms And Collision Term Is Computed In One Step With A Multi-scale Scheme Without Splitting. The Ugks Also$100K
Feb 2011Federal contractNASA · Zona Technology, Inc. Proposes An R&d Effort To Develop An Adaptive Flight Control System Which Can Provide Near-nominal Performance For The Aircraft Under Off-nominal Conditions, Consequently Reduce Pilot-vehicle Interactions. Furthermore, This Adaptive Control System Is Combined With A Monitoring System To Detect Possible Pilot-induced Oscillation (pio) While Both Pilot And Controller Are Adaptively Working, In Order To Avoid Pio And Enhance Aviation Safety. The Proposed Comprehensive Combined$100K
Feb 2011Federal contractNASA · Zona Technology, Inc. (zona) Proposes An R\&d Effort To Develop An Experimental Model Based Feedback Control (embfc) Framework For The Flutter Suppression And Gust Load Alleviation (gla). The Resilience Of The Flight Control Law In The Presence Of Aeroelastic/aeroservoelastic (ae/ase) Interactions Can Therefore Be Increased By The Suppression Of The Aircraft's Structural Vibrations Induced By The Flutter Mechanism And/or Gust Perturbation. Currently Aircrafts With Non-adaptive Control Laws Usual$100K
Aug 2010Federal contractNASA · Multiscale Gaskinetics/particle (mgp) Simulation For Rocket Plume/lunar Dust Interactions An Efficient And Accurate Software Package Named Zmgp (zona Multi-scale Gaskinetic/particle Simulation Package) Is Proposed As A 3D Tool To Predict The Lunar Dust Trajectory And Crater Formation Process When A Retro-rocket Lands On The Lunar Surface. Zmgp Has Many Special Features Including: 1, The Hybrid Flow Module By Coupling The Gaskinetic Bhatnagar-gross-krook (bgk) Model And The Direct Simulation Mont$600K
Apr 2010Federal contractDefense · Zaero Software Renewal$41K
Mar 2010Federal contractNASA · Zaero Software Renewal$24K
Jan 2010Federal contractNASA · Multidisciplinary Design And Optimization (mdo) Tools Developed To Perform Multi-disciplinary Analysis Based On Low Fidelity Computation Methods Have Been Used In Aircraft Conceptual Design For Decades. These Tools Have Been Proven Very Effective For Simple Problems And Mostly Have Been Developed As A Single Codes. However, As Analyses Have Become More Complex And The Need To Consider More Design Factors Crucial, Such Codes Have Grown So Large As To Be Inconceivable And Difficult To Maintain. No$100K
Jan 2010Federal contractNASA · Zona Technology, Inc. (zona) Proposes To Develop An On-line Flutter Prediction Tool For Wind Tunnel Model Using The Parameter Varying Estimation (pve) Technique To Ensure The Safety Of The Flutter Model As Well As The Wind Tunnel System. This Tool Will Be Applied To Rapidly Evaluate Parameters, Such As Modal Damping And Frequency, Which Are Required To Assess The Flutter Boundary Of A Wind Tunnel Model In The Pre-flutter Test Conditions. In This Pve Toolbox, System Identification Techniques Such$100K
Jan 2010Federal contractNASA · TAS::80 0121::TAS Multidisciplinary Design, Analysis, And Optimization (mdao) Tools Today Possess Limited Disciplines With Little Fidelity Modeling Capability. These Tools Are Typically Developed As A Single Large Software Application That Performs Analysis For All Disciplines But Has Little Or No Capability To Integrate Multi-fidelity And Multi-discipline Components That Have Already Been Developed As Stand-alone Analysis Codes. Even Though A Multitude Of Tools Have Been Developed And Well Adap$100K
Jan 2010Federal contractNASA · Zona Technology, Inc. (zona) Proposes To Develop An Integrated Flight Dynamics Simulation Capability With Nonlinear Aeroelastic Interactions By Combining A Flight Dynamics Model And An Added-on Nonlinear Aeroelastic Solver In A Simulink Environment. This Nonlinear Aeroelastic Solver Is Generated By Interacting A Nonlinear Structural Reduced Order Model (rom) With A Neural-network-based (nn-based) Aerodynamic Rom, Called The Rom-rom Procedure, To Provide The Incremental Aeroelastic Forces And Mom$100K
Dec 2009Federal contractNASA · Cfd-based Design-oriented (do) Steady/unsteady Aerodynamic Analysis Tools For Aeroelastic / Aeroservoelastic (ae/ase) Evaluation Lag Significantly Behind Other Multidisciplinary Design Optimization (mdo) Developments For Flight Vehicle Design. In Practically All Studies To Date Involving Configuration Multidisciplinary Shape Optimization, Dynamic Ae/ase Constraints Were Left Out, Thus, Rendering The Design Results Incomplete. Flutter, Gust Stresses, Vibration, Fatigue, Ride Comfort, Handling Qua$600K
Sep 2009Federal contractDefense · A System Approach Using Carteuler-based Nonlinear Aeroelasti$791K
Jun 2009Federal contractNASA · Zona Technology, Inc (zona) And Arizona State University (asu) Propose A R&d Effort To Further Develop The Ground Flutter Testing System In Place Of A Wind Tunnel (wt), Called The Dry Wind Tunnel (dwt) System. The Dwt System Consists Of A Ground Vibration Test (gvt) Hardware System And A Real-time Unsteady Aerodynamic Force Generation Software System Developed From An Aerodynamic Reduced Order Model (rom). The Dwt System Can Serve As A Replacement Or Complimentary Means For Flutter/ase Instabil$600K
Apr 2009Federal contractNASA · Zaero Option III, Ase Option, Trim Oprion License Renewal$24K
Apr 2009Federal contractNASA · Zonair Option III Annual License$15K
Feb 2009Federal contractNASA · Nonlinear Aerodynamic And Nonlinear Structures Interations (nansi) Methodology For Ballute/inflatable Aeroelasticity In Hypersonic Atmospheric Entry Technical Abstract: Zona Proposes A Phase II Effort To Fully Develop A Comprehensive Methodology For Aeroelastic Predictions Of The Nonlinear Aerodynamic/aerothermodynamic - Structure Interaction (nansi) On Ballutes During Hypersonic Atmospheric Entry, Including Potential Surface Wrinkling. A Time-accurate Boltzmann Aerodynamic Flow Solver, Called$600K
Feb 2009Federal contractNASA · Adaptive Feedfoward Feedback Control Framework An Adaptive Feedforward And Feedback Control (affc) Framework Is Proposed To Suppress The Aircraft's Structural Vibrations And To Increase The Resilience Of The Flight Control Law, In The Presence Of Ae/ase Interactions. Specifically, The Adaptive Feedforward Controller Is Designed To Reduce Any Atmospheric Induced Structural Vibrations Of The Aircraft. The Adaptive Feedback Controller Is Applied As An Additive Perturbation Of The Flight Control Sy$600K
Jan 2009Federal contractNASA · A Unified Multi-dimensional Gaskinetic Hybrid Bgk-dsmc Method For Nonequilibrium And Chemically Reacting Flows A Consistent And Accurate Hybrid Gaskinetic Bgk And Dsmc Method, Valid In The Full Knudsen Number (kn) Range, Is Proposed As A 3D Tool To Handle Hypersonic Aerothermodynamics From Continuum To Thermochemical Nonequilibrium And Ionized/plasma Flows. By Domain-decomposition, The Proposed Method Will Provide Adjoint But Automated Sub-domain Solutions By Solving The Gaskinetic Bgk Method O$100K
Jan 2009Federal contractNASA · Multiscale Gaskinetics/particle (mgp) Simulation For Rocket Plume/lunar Dust Interactions A Multiscale Gaskinetic/particle (mgp) Computational Method Is Proposed To Simulate The Plume-crater-interaction/dust-impingement(pcidi) Problem. The Mgp Method Consists Of A Multiscale Gaskinetic (mg) Method For Gasdynamics Of Rocket Plume-in-vacuum Flowfield, An Overlay Method For Gas-particle Interaction. Mg Combines Bgk Gaskinetics (bgk) And Direct Simulation Monte Carlo (dsmc) Methods With A Domain D$100K
Jan 2009Federal contractNASA · Zeus-do: A Design Oriented Cfd-based Unsteady Aerodynamic Capability For Flight Vehicle Multidisciplinary Configuration Shape Optimization In Practically All Air-vehicle Mdo Studies To Date Involving Configuration Shape Optimization, Dynamic Aeroservoelastic Constraints Had To Be Left Out. Flutter, Gust Stresses, Vibration, And Ride Comfort Cannot Still Be Accounted For In Mdo Involving Configuration Shape Variations. Development Of The Missing Mdo Building Block Is Proposed Here: A Design-ori$100K
Jan 2009Federal contractDefense · Zaero Software$41K
Nov 2008Federal contractDefense · STTR Phase I - (ffp) Guiding Action$100K
Sep 2008Federal contractDefense · Zaero Software.$41K
Jul 2008Federal contractNASA · Sap Purchase Requisition: 4200258793 Zonair III$15K
Apr 2008Federal contractNASA · Sap Purchase Requisition: 4200239209 Zaero Option Software Renewal$24K
Jan 2008Federal contractNASA · Nonlinear Aerodynamic Rom-structural Rom Methodology For Inflatable Aeroelasticity In Hypersonic Atmospheric Entry$100K
Jan 2008Federal contractNASA · Adaptive Feedforward Feedback Control Framework$100K
Jan 2008Federal contractNASA · Zona Technology Inc (zona) And Arizona State University (asu) Propose A R&d Effort To Develop A Ground Flutter Testing System Without Wind Tunnel Called The Dry Wind Tunnel (dwt) System. The Dwt System Consists Of A Ground Vibration Test (gvt) Hardware System And A Real-time Unsteady Aerodynamic Force Generation Software Developed From An Aerodynamic Reduced Order Model (rom). The Ground Flutter Test Using The Dwt System Operates On The Real Structural Model Thereby No Scale-down Structural Mode$100K
Nov 2007Federal contractNASA · Sap Purchase Requisition: 4200224956 Flutter Analysis Of The Modified 747 Sofia Model$26K
Oct 2007Federal contractDefense · STTR Phase 2$927K
Sep 2007Federal contractNASA · Cfd-based Aeroservoelastic Methodology For Supersonic Aircraft Flutter Suppression Gust Loads Alleviation,& Ride Quality Augmentation (nra Proposal #06-SUP2-06-0015) **** This Sow Defines The Requirements For Developing And Demonstrating A Methodology For Aeroservoelastic (ase) Control Law Design, Based On The Proposed High-level Cfd Tool Carteuler. This Methodology Shall Be Applied To The Supersonic Semi-span Transport (S4T) Wind-tunnel Model To Simultaneously Suppress Flutter (fs), Alleviate $419K
Jun 2007Federal contractDefense · Phase II - Optimization Of Parameter Id For Flut$596K
Mar 2007Federal contractDefense · STTR Phase 2 ($550K To $750K) Inc Funding/no Opt Cpff$750K
Oct 2005Federal contractDefense · 200603!000005!5700!FA9550!AFOSR/PK !FA955006C0003 !a!n! !y! ! !20051017!20071031!182103291!182103291!182103291!N!ZONA Technology, Inc !9489 E Ironwood Square Dr !scottsdale !AZ!85258!65000!013!04!SCOTTSDALE !maricopa !arizona !+000000373227!N!N!000000746454!AJ16!RDTE/PHYSICAL Sciences - Management Support !S1 !services !000 !not Discernable !541710!E! !3! ! ! ! ! !999$746K
Feb 2004Federal contractDefense · 200402!000198!2100!W31P4Q!USA Aviation And Missile COMMAND!W31P4Q04CR045 !a!n! !n! ! !20031107!20051130!182103291!182103291!182103291!N!ZONA Technology Inc !7430 E Stetson Drive Suite!scottsdale !AZ!85251!65000!013!04!SCOTTSDALE !maricopa !arizona !+000000373184!N!N!000000000000!AJ12!RDTE/PHYSICAL Sciences - Applied Research !A2 !missile And Space Systems !000 !* !541511!E! !3! ! ! ! ! !999$717K

Federal awards are summed by year (109 awards); hover a bar for the split. Form D reports securities sold, which can differ from an announced round; filings are numbered in the order they were made.

1 record has no date or no amount, so it isn’t placed on the timeline.

Standing among 44 peers

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Aerospace · Software

Federal grants#5 · top 11%

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Checked: USPTO inventors; federal award principal investigators; SEC Form D related persons · Oct 23, 2026

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What it has protected

No granted patents are on record.

USPTO usually publishes applications 18 months after filing, so recent applications may not be visible yet. Patents assigned under a different entity name won’t match.

Checked: USPTO granted patents and published applications · Oct 23, 2026

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Regulatory activity · Aerospace

Sector-level, not company-level

06 Jul 2026Nondiscrimination in Federally Assisted Programs of NASA-Effectuation of Title VI of the Civil Rights Act of 1964National Aeronautics and Space Administration
01 Jul 2026Special Conditions: AMAC Aerospace, The Boeing Company Model 747- 8 Airplane; Side-Facing SeatsFederal Aviation Administration
26 Jun 2026Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous AmendmentsFederal Aviation Administration
23 Jun 2026Operating Limitations at John F. Kennedy International AirportFederal Aviation Administration
23 Jun 2026Operating Limitations at New York LaGuardia AirportFederal Aviation Administration
18 Jun 2026Special Conditions: Honeywell Aerospace US LLC, Dassault Aviation Model Falcon 900EX Airplane; Electronic System Security Protection From Unauthorized External AccessFederal Aviation Administration

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Sources

Federal grants from SBIR/STTR, NIH, NSF and DoD records. Federal contracts from USAspending.gov. Private capital from SEC Form D. Patents from USPTO. Publications from OpenAlex. Regulatory activity from the Federal Register. Press matched on company name.

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Data freshness

SEC Form D filings through Oct 23, 2026. SBIR and STTR awards through Oct 21, 2026.