M4 ENGINEERING, INC.
Grid adaptation algorithm for computational fluid dynamics using Dynamic Mode Decomposition to dynamically optimize unstructured meshes for hypersonic flow simulations
- Sector
- Aerospace
- Headquarters
- Long Beach, CA
- Total capital
- $48.8M
- Federal grants
- $11M
- 19 awards · 2016–2026
- Rank in peer group#16 of 55
- Private capital raised
- None on recordNo Form D filings on SEC EDGAR. Some raises are not filed.
- Federal contracts
- $37.7M
- 77 awards · Defense, NASA, General Services A
- Rank in Aerospace#97 of 1335
- Granted patents
- None on recordNo USPTO grants. Applications publish after 18 months.
Capital timeline
Latest events
- Federal grantNASA · Phase I · SBIR Phase I Agentic Framework For Precision Composite Optomechanical Hardware$225K
- Federal grantDefense · Phase II · SBIR Ph 2 Advanced Carbon-carbon Composites For Aerospace Structures$4.9M
- Federal grantDefense · Phase I · Research And Development.$140K
- Federal contractDefense · Research And Development.$140K
- Federal contractNASA · SBIR I PYFOIL81: Rotorcraft Design Tool Airfoil Table Generator$150K
- Federal contractDefense · A As Landing Gear Engineering Services Analysis$1.9M
- Federal grantNASA · Phase I · SBIR I PYFOIL81: Rotorcraft Design Tool Airfoil Table Generator$150K
Show 89 earlier federal awards
- Federal grantNASA · Phase II · Phase II SBIR 80NSSC25C0005 Uam Design Space Exploration Framework With Embedded Version Control$850K
- Federal contractNASA · Phase II SBIR 80NSSC25C0005 Uam Design Space Exploration Framework With Embedded Version Control$850K
- Federal grantDefense · Phase I · Research And Development.$140K
- Federal contractDefense · Research And Development.$140K
- Federal contractNASA · FY24 SBIR Phase I- Uam Design Space Exploration Framework With Embedded Version Control$150K
- Federal grantNASA · Phase I · FY24 SBIR Phase I- Uam Design Space Exploration Framework With Embedded Version Control$150K
- Federal grantDefense · Phase II · STTR Phase II R&d$1.5M
- Federal contractDefense · STTR Phase II R&d$1.5M
- Federal grantNASA · Phase II · STTR Phase II Topology Optimization For Design Of Highly Tailored Composites For Afp Manufacturing$850K
- Federal contractNASA · STTR Phase II Topology Optimization For Design Of Highly Tailored Composites For Afp Manufacturing$850K
- Federal contractNASA · NASA Model-based Systems Analysis And Engineering (mbsa&e) For The Sustainable Flight National Partnership (sfnp) Phase 1$450K
- Federal contractDefense · Research And Development$1.3M
- Federal grantNASA · Phase I · Unsteady Metric-based Adaptation via Koopman Expansion of the Feature Field$150K
- Federal grantDefense · Phase I · Friction Drilling Fasteners for Composite Structures$140K
- Federal grantDefense · Phase I · Low Cost Carbon-Carbon Development for Hypersonic Flight Systems$150K
- Federal grantDefense · Phase I · Resin Process Research & Scale-up for Aerospace Carbon-Carbon Composite Structures$100K
- Federal contractDefense · Basic Research & Development Dha Phase II SBIR 21.1 Project Titled, Underwater Blast Lung Computational Model$1.1M
- Federal grantNASA · Phase I · Topology Optimization for Design of Highly Tailored Composites for AFP Manufacturing$150K
- Federal contractDefense · SBIR Phase I$240K
- Federal contractDefense · Physics-based Structural Analysis Model Development And Integration With Computational Aircraft Prototype Syntheses$1.2M
- Federal contractDefense · Medical Research And Development Dha SBIR Ph I H211-003-0280$250K
- Federal contractNASA · Ot Aeroelasticity And Aeroservoelastic Control$750K
- Federal grantNASA · Phase I · Design Tools for Advanced Tailorable Composites$125K
- Federal grantNASA · Phase I · Low Cost Carbon-Carbon Composites for Hot Structures$125K
- Federal contractNASA · Generative Adversarial Networks For Real-time Realistic Physics Simulations$1.1M
- Federal contractNASA · Aeroelasticity And Aeroservoelastic Control$125K
- Federal grantNASA · Phase I · Advanced Propulsion Systems Ground Test Technology$125K
- Federal contractDefense · Finite Element Method (fem) For Bonded Repair Design$150K
- Federal grantDefense · Phase I · Hexahedral Dominant Auto-Mesh Generator$140K
- Federal contractNASA · Novel Ase Scaled Model Design, Fabrication, And Testing$1.1M
- Federal contractNASA · Physics-based Conceptual Design Tools$502K
- Federal contractNASA · Lightweight Conformal Structures$125K
- Federal contractDefense · Vvtm Software Upgrade$72K
- Federal contractDefense · Igf::ot::igf Research And Development$1.0M
- Federal contractDefense · STTR Phase I Research&development - Uncertainty Reduction In High Speed Flight Vehicle Modeling$100K
- Federal contractDefense · Microstructurally-based Constitutive Models For Composite Energetic Materials$150K
- Federal contractNASA · In The Current Proposal, M4 Engineering Will Continue To Modernize And Enhance The Pbweight Software To Support Rotorcraft Features And Applications. Various Updates Will Be Made To The Software Package To Support Deployment On The Windows 10 Operating System. Additionally, Effort Will Be Placed On Reducing The Dependency On Opencascade And The Delivered Package Will Only Include Libraries That Are Utilized By The Tool. A Series Of Important Bug Fixes Will Also Be Addressed In The Current Effort$519K
- Federal contractNASA · We Propose The Demonstration Of A Novel Aeroservoelastic Scaled Model Design, Optimization, And Fabrication Approach Combining Aeroservoelastic Scaling With A Combined Topology/sizing Optimization To Match The Target Structural Dynamic And Aeroelastic Behavior. Fabrication Is Using 3D Printing Techniques (metal And Plastic/elastomer), Along With Automated Electronic Assembly Techniques For In-situ Instrumentation. A Scaled Model Will Be Designed, Fabricated, And Tested In A Low Speed Wind Tunnel$125K
- Federal contractDefense · Extremely Small Balance Technology$150K
- Federal contractDefense · Air Force Rapid Innovation Fund - Advanced Analytics To Support Weapons Certification For 5TH/6TH Generation Platforms$1.2M
- Federal contractGeneral Services A · Igf::ot::igf - Darpa SBIR Phase I D172-002 Research&development Award.$175K
- Federal contractDefense · Igf::ot::igf Status Report$230K
- Federal contractNASA · Igf::ot::igf We Propose The Development Of A Novel Aerodynamic Modeling Approach Making Use Of Fully Unstructured Grids For Unsteady Panel Aerodynamic Models For Aeroelastic And Aeroservoelastic Analysis. The Unsteady Aerodynamic Code Will Be Integrated With An Existing Suite Of Aeroelastic And Aeroservoelastic Analysis Tools Making It Possible To Perform Aeroelastic And Aeroservoelastic Analysis Of Complex Vehicles With A Significant Reduction In User Effort And Improvement In Fidelity.$750K
- Federal grantDefense · Phase II · Bonded Joint Analysis Method$911K
- Federal contractDefense · Research And Development, Igf::ot::igf$1.4M
- Federal contractNASA · Igf::ot::igf M4 Engineering Proposes To Develop Methods And Software To Generate Reduced Order Nonlinear Models Of Dynamic Aeroserovelastic Systems. The Reduced Order Models Will Be Based On A Hybrid Narmax-wavelet Model, In Which The Basic Linear Behavior And Gentle Nonlinearities In The Dynamics Are Captured By A Nonlinear Autoregressive, Moving Average With Exogenous Inputs (narmax) Model With Polynomial Behavior, And Harsh Nonlinearities That Result Localized Discontinuities Or Transitions $125K
- Federal contractDefense · Igf::ot::igf Ph III SBIR- Ixgen Software Improvement$250K
- Federal contractNASA · Igf::ot::igf We Propose The Development Of A Modern Panel Code For Calculation Of Steady And Unsteady Aerodynamic Loads Needed For Dynamic Servoelastic (dse) Analysis Of Flight Vehicles. The Code Will Be Especially Tailored To Be Robust, Reliable, And Integrated With The NASA Object Oriented Optimization (O3) System Through Selection Of Analysis Methods, File Formats, And Computing Environment, Allowing It To Be Efficiently Applied To Numerous Problems Of Interest To NASA And Industry.$125K
- Federal contractNASA · Igf::ot::igf M4 Engineering And Missouri S&t Propose To Investigate The Viability Of Creating A Multidisciplinary Analysis And Optimization Architecture For Analyzing Spacecraft System Models. The Current Approach Will Utilize Commercial Off-the-shelf (cots) Software To Alleviate Acquisition Hurdles For NASA (and Public) Technical Monitors/reviewers. Next, A Preliminary Set Of Analysis Modules Will Be Developed Including A Cad-based Geometry Component Capable Of Generating Parametric Geometry. O$122K
- Federal contractDefense · Igf::ot::igf SBIR I Uncertain Propagation Modal Parameters$150K
- Federal contractNASA · Igf::ot::igf In Aircraft Design, Reducing Structural Weight Is Often A Prime Objective, While Various Constraints In Multiple Disciplines, Such As Structure, Aerodynamics And Aeroelasticity Should Be Imposed On The Aircraft. Therefore, Engineers Need Optimization Tools To Incorporate The Multidisciplinary Constraints Using Appropriate Fidelity During The Early Stages Of Concept Design. Classic Structural Design Of Aircraft Structures Is Based On The Concept Of A "wing Box" That Uses Simple Comp$750K
- Federal contractNASA · Igf::ot::igf Approaches For Weight Prediction, In The Conceptual Design Phase, Typically Consist Of Parametric Relations Or Empirical Databases. Historical Databases Work Reasonably Well When Applied To Existing Or Conventional Designs, However, They Fail To Predict Accurately The Weights And Loads Associated With Unconventional Designs (like The Low Boom Flight Demonstrator). There Exists A Need To Augment Existing Historical Databases With A Physics-based Methodology/capability For Predicting $750K
- Federal contractDefense · Igf::ot::igf Evaluation Of Unsteady Loading On Store Trajectories SBIR II$1.5M
- Federal contractNASA · Igf::ot::igf M4 Engineering Proposes To Conduct Canonical Aeroelastic Benchmark Experiments. These Experiments Will Augment Existing Sources For Aeroelastic Data In The Transonic Regime. Models Will Be Constructed With Well Characterized Engineering Materials And Will Include Measurement Of High Frequency Pressure Data. A Variety Of Transonic Conditions Will Be Tested To Provide Opportunities For Validation Of Aeroelastic Response Of Transonic Flows Not Previously Available.$125K
- Federal contractNASA · Igf::ot::igf In The Current Proposal, M4 Engineering Will Develop And Evaluate The Feasibility Of An Innovative Concept Aimed At Enhancing Previously Developed Databases With Physicsbased Weight And Load Estimation Relationships (via Stochastic Response Surfaces) For Unconventional (and Conventional!) Conceptual Wing And Fuselage Designs. The Main Goal For This Effort Will Be To Develop A Software Tool Capable Of Generating Weight And Load Responses For Unconventional Designs From Physics-based $125K
- Federal contractNASA · Igf::ot::igf We Propose Development And Demonstration Of A Dynamic Aeroservoelastic Modeling And Optimization System Based On Curvilinear Internal Structural Arrangements Of Variable Topology. This Will Allow Combined Sizing And Topology Optimization Of Complete Airplane Configurations Including Aeroservoelastic Performance.$124K
- Federal contractDefense · STTR N12A-T004$750K
- Federal contractDefense · Igf::ot::igf Evaluation Of Unsteady Loading On Store Tragjectories$150K
- Federal contractDefense · N13A-T002$80K
- Federal contractDefense · Igf::ot::igf Innovative Propeller&open-rotor Propulsion Multi-point Multi-disciplinary Optimization$150K
- Federal contractDefense · Ph I Research&development Titled: M&s Uncertainty Quantification. Igf::ot::igf$100K
- Federal contractDefense · Igf::ot::igf AF112-187 Wind Tunnel Balance Correction For Structual Steel Motion Effects$950K
- Federal contractDefense · Topic N12A-T004$150K
- Federal contractDefense · SBIR P2 Topic AF093-214 Store Unsteady Aerodynamic Loads Measurement Technology$870K
- Federal contractDefense · SBIR Phase I Topic AF112-187, Proposal 2039, Wind Tunnel Balance Correction For Structural Motion Effects$125K
- Federal contractNASA · The Objective For The Phase II Effort Will Be To Develop A Comprehensive, Efficient, And Flexible Uncertainty Quantification (uq) Framework Implemented Within A Matured User-friendly Software, Which Will Enable The Modeling Of Both Inherent And Epistemic Uncertainties In Spacecraft System Models, Have A General Quantification Of Margins And Uncertainties (qmu) Capability For System Certification And Reliability Assessment, And Utilize Advanced Methods Based On Non-intrusive Polynomial Chaos (nip$600K
- Federal contractDefense · Topic N101-015 Virtual Vibration Of External Stores$750K
- Federal contractDefense · Topic Af 093-214, Proposal F093-214-1491$100K
- Federal contractDefense · SBIR Phase 1 Topic # N101-015$150K
- Federal contractNASA · The Proposed Effort Is To Investigate A Novel Uncertainty Quantification (uq) Approach Based On Non-intrusive Polynomial Chaos (nipc) For Computationally Efficient And Accurate Quantification Of Uncertainties In Spacecraft System Models Within A Multidisciplinary Analysis And Optimization (mao) Framework. The Uq Approach Will Include The Modeling Of Both Inherent (probabilistic) And Epistemic Uncertainties And The Propagation Of These With Nipc. Comparisons Between Crude Monte-carlo Sampling Wil$100K
- Federal contractNASA · During Phase I, M4 Engineering Integrated A Prototype System Into Openmdao, A NASA Grc Open-source Framework. This Prototype System Was A Proof-of-concept That M4 Physics Based Modules Could Be Integrated In Openmdao. The Results Generated In Openmdao Compared Well To The Results Generated In Another Framework, Modelcenter. Phase II Will Be A Demonstration Of Enhanced System Functionality With The Integration Of Additional Modules And Design Tools. The Integrated Objects Will Perform Discipline-$600K
- Federal contractDefense · SBIR Phase 1, Topic #A09-140$70K
- Federal contractDefense · Store Trajectory Response To Unsteady Aerodynamic Loads$750K
- Federal contractNASA · Generalized Reduced Order Model Generation Technical Abstract M4 Engineering Proposes To Develop A Generalized Reduced Order Model Generation Method. This Method Will Allow For Creation Of Reduced Order Aeroservoelastic State Space Models That Can Be Interpolated Across A Range Of Flight Conditions. This Development Will Be A Significant Advance To The Process Of Control Law Development, Especially In The Design Of Control Systems Required To Provide Flutter Suppression, Gust Load Alleviation,$600K
- Federal contractNASA · Integrated Multidisciplinary Optimization Objects M4 Engineering Proposes To Implement Physics-based, Multidisciplinary Analysis And Optimization Objects That Will Be Integrated Into A Python, Open-source Framework And Used In A Wide Variety Of Simulations. The Integrated Objects Will Perform Discipline-specific Analysis Across Multiple Flight Regimes At Varying Levels Of Fidelity. The Process Will Also Deliver System-level, Multi-objective Optimization. Addressing Physics-based, System-level O$99K
- Federal contractDefense · Advanced Composite Damage And Repair Evaluation System$100K
- Federal contractDefense · SBIR I$100K
- Federal contractNASA · Generalized Reduced Order Model Generation$100K
- Federal contractNASA · M4 Engineering Proposes The Development Of An Adaptive Structural Mode Control System. The Adaptive Control System Will Begin From A Baseline Dynamic Model Of The System Which Will Be Updated As The System Is Operated. This Allows The Control Inputs To Be Tailored To The Observed Behavior Of The System Across A Range Of Flight Conditions Weight Conditions And Failure Conditions While Accounting For Uncertainty In Structural Dynamics And Aerodynamics. The Development Of The Adaptive Control Syste$100K
- Federal contractNASA · Optimization Of Weight Including Damage Scenarios$100K
- Federal contractNASA · Sap Purchase Requisition: 4200228264. Funding For SBIR, Subtopic Air Craft Systems Analysis, Design And Optimization. Title: Multidisciplinary Optimization Object Library.$599K
- Federal contractDefense · Ph I SBIR Topic A07-176, Advanced System Level Durability Analysis, Prediciton, And Optimization$70K
- Federal contractNASA · The Supersonics Project Is Aligned With The Armd Principals Of Maintaining Intellectual Stewardship Of Aeronautical Core Competencies For The Nation In The Supersonic Flight Regime And Of Focusing Research In Areas That Are Appropriate To Nasas Unique Capabilities. The Supersonics Project Is A Broad Based Effort Designed To Develop Knowledge, Capabilities And Technologies That Support All Vehicles That Fly In The Supersonic Speed Regime. From This Broad Spectrum, The Project Has Selected Two C$1.2M
- Federal contractNASA · Nra Award Entitled Simultaneous Flutter Suppression, Gust Load Alleviation, And Ride Quality Augmentation For Supersonic Aircraft At Transonic Conditions. A Major Focus Of This Nra Is To Encourage Collaboration Between Other Organizations And NASA To Help Achieve Specific Goals In A Variety Of Foundational Aeronautics Research Programs. The Research Programs Of Nasa's Armd Consists Of Four Programs; The Fundamental Aeronautics Program, The Aviation Safety Program, The Airspace Systems Program A$600K
- Federal contractDefense · Geometry Manipulation Through Automated Parameterization$911K
- Federal contractDefense · 200612!005552!2100!W31P4Q!USA Aviation And Missile COMMAND!W31P4Q06C0486 !a!n! !n! ! !20060913!20080830!133626544!133626544!133626544!N!M4 Engineering Inc !2161 Gundry Ave !signal Hill !CA!90755!71876!037!06!SIGNAL Hill !los Angeles !CALIFORNIA!+000000364993!N!N!000000000000!AD92!RDTE/OTHER Defense-applied Research !A2 !missile And Space Systems !000 !not Discernable !541710!E! !3! ! ! ! ! !999$727K
- Federal contractDefense · 200511!000271!5700!FA9300!AFFTC/PKT !FA930005D0011 !a!n! !Y!0001 ! !20050826!20060801!133626544!133626544!133626544!N!M4 Engineering Inc !2161 Gundry Ave !signal Hill !CA!90755!71876!037!06!SIGNAL Hill !los Angeles !CALIFORNIA!+000000020000!N!N!000000000000!AC21!RDTE/MISSILE And Space Systems-basic Research !A2 !missile And Space Systems !000 !* !541710!E! !5!B!M! !a! !202$47K
- Federal contractDefense · 200509!002370!5700!FA8650!DET 1 Afrl/pk !FA865005C3537 !a!n! !n! ! !20050608!20071008!133626544!133626544!133626544!N!M4 Engineering Inc !2161 Gundry Ave !signal Hill !CA!90755!71876!037!06!SIGNAL Hill !los Angeles !CALIFORNIA!+000000150000!N!N!000000749953!AC15!RDTE/AIRCRAFT-ENG/MANUF Develop !A2 !missile And Space Systems !248 !minuteman III Prp !332812!E! !3! ! ! ! ! !202$850K
- Federal contractDefense · 200503!000508!2100!W31P4Q!USA Aviation And Missile COMMAND!W31P4Q05CR035 !a!n! !n! ! !20041222!20051231!133626544!133626544!133626544!N!M4 Engineering Inc !2161 Gundry Ave !signal Hill !CA!90755!43000!037!06!LONG Beach !los Angeles !CALIFORNIA!+000000364977!N!N!000000000000!AD92!RDTE/OTHER Defense-applied Research !A2 !missile And Space Systems !000 !* !541710!E! !3! ! ! ! ! !202$857K
Federal awards are summed by year (96 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.
Standing among 55 peers
Line = medianAerospace · Software
- Federal grants#16 · top 29%
Cumulative measures favor older companies. Rankings describe position today, not outcome. Below the median, ranks show as a band rather than a number.
Founders and team
No founders are linked to this company yet.
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Checked: USPTO inventors; federal award principal investigators; SEC Form D related persons · Oct 23, 2026
Claim this profile to add your teamWhat 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
- Nondiscrimination in Federally Assisted Programs of NASA-Effectuation of Title VI of the Civil Rights Act of 1964National Aeronautics and Space Administration
- Special Conditions: AMAC Aerospace, The Boeing Company Model 747- 8 Airplane; Side-Facing SeatsFederal Aviation Administration
- Standard Instrument Approach Procedures, and Takeoff Minimums and Obstacle Departure Procedures; Miscellaneous AmendmentsFederal Aviation Administration
- Operating Limitations at John F. Kennedy International AirportFederal Aviation Administration
- Operating Limitations at New York LaGuardia AirportFederal Aviation Administration
- Special 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.
How to read this page
Figures show associations in public records, not causes or predictions. Nothing here is investment advice. An em-dash means no record was found under this company's name, not that none exists.
Data freshness
SEC Form D filings through . SBIR and STTR awards through .