MATERIALS RESEARCH & DESIGN INC
Ceramic matrix composite (CMC) materials for hypersonic and re-entry applications with oxidation resistance
- Sector
- Materials
- Headquarters
- Wayne, PA
- Total capital
- $113M
- Federal grants
- $34.4M
- 47 awards · 2014–2025
- Rank in peer group#3 of 84
- Private capital raised
- None on recordNo Form D filings on SEC EDGAR. Some raises are not filed.
- Federal contracts
- $78.4M
- 125 awards · Defense, NASA, Federal Election C
- Rank in Materials#6 of 1258
- Granted patents
- None on recordNo USPTO grants. Applications publish after 18 months.
Capital timeline
Latest events
- Federal grantDefense · Phase II · Domestically Available Ablative Materials - Phase II$3.4M
- Federal contractDefense · Domestically Available Ablative Materials - Phase II$3.4M
- Federal contractNASA · SBIR I 3D Reinforced Composites For Improved Impact Resistance In Spacesuits$150K
- Federal grantNASA · Phase I · SBIR I 3D Reinforced Composites For Improved Impact Resistance In Spacesuits$150K
- Federal contractDefense · Research And Development To Establish A Computational Network For The Optimization Of Pyrolysis Processes To Be Used For Advanced Manufacturing Of Carbon-carbon Composites.$1.3M
- Federal grantDefense · Phase II · Research And Development To Establish A Computational Network For The Optimization Of Pyrolysis Processes To Be Used For Advanced Manufacturing Of Carbon-carbon Composites.$1.3M
- Federal contractDefense · Materials Research & Design: SBIR Phase II Proposal NUMBER:L2S-0059 Proposal Title: High-temperature Composite Nozzle Extensions For Space Access And Propulsion Topic NUMBER:DLA23A-003$1.9M
Show 165 earlier federal awards
- Federal grantDefense · Phase I · Sbir/sttr Phase I Research & Development Laser Heated Tensile Test Method$150K
- Federal contractDefense · Sbir/sttr Phase I Research & Development Laser Heated Tensile Test Method$150K
- Federal grantDefense · Phase I · Sbir/sttr Phase I Research & Development Silicide Coatings For Surface Morphing Interceptors$150K
- Federal contractDefense · Sbir/sttr Phase I Research & Development Silicide Coatings For Surface Morphing Interceptors$150K
- Federal contractDefense · Large Form-factor Ox/ox Window For Hypersonic Seekers$1.8M
- Federal grantDefense · Phase II · Large Form-factor Ox/ox Window For Hypersonic Seekers$1.8M
- Federal contractDefense · Gleam_mr_d$1.4M
- Federal contractDefense · The Contractor Shall Provide The Requirements In STTR Phase 1 And Final Report In Accordance With Proposal A23B-T011-0042 Dated 06/14/2023. The Government's Terms And Conditions Shall Apply.$197K
- Federal grantDefense · Phase I · The Contractor Shall Provide The Requirements In STTR Phase 1 And Final Report In Accordance With Proposal A23B-T011-0042 Dated 06/14/2023. The Government's Terms And Conditions Shall Apply.$197K
- Federal grantDefense · Phase II · STTR Phase II Materials Research & Design Proposal L2-0450 Titled "a Material Model For N-dimensionally Reinforced High- Temperature Composites".$1.8M
- Federal contractDefense · STTR Phase II Materials Research & Design Proposal L2-0450 Titled "a Material Model For N-dimensionally Reinforced High- Temperature Composites".$1.8M
- Federal contractDefense · Analyze Specified Mach 8 Hardware At Arnold Engineering Complex (aedc) Hypervelocity Wind Tunnel Number 9 Facility$40K
- Federal grantDefense · Phase II · Sbir/sttr Phase II R&d$1.5M
- Federal contractDefense · Sbir/sttr Phase II R&d$1.5M
- Federal contractDefense · Analyze Specified Mach 14 Hardware At Arnold Engineering Development Complex (aedc) Hypervelocity Wind Tunnel No. 9 Facility$75K
- Federal contractDefense · Production Readiness For Complex Carbon-carbon Assemblies For Hypersonic Glide Aeroshells$1.7M
- Federal grantDefense · Phase II · A C/SiC Damage Model for Extreme Environments$1.2M
- Federal grantDefense · Phase II · Refractory Ceramic Matrix Composites for Shape-Stable Nosetips$1.2M
- Federal grantDefense · Phase I · A Generalized Model for Assessing Manufacturability of 2D and 3D Reinforced High-Temperature Composites$100K
- Federal grantDefense · Phase II · Domestic Needled Preforms for C/SiC Composites$500K
- Federal contractDefense · SBIR Phase II - L2D-0110$1.0M
- Federal grantDefense · Phase II · A Digital Twin Model for Robust 3D Woven PMC Pi Joints$1.0M
- Federal contractDefense · Research And Development$2M
- Federal grantDefense · Phase I · Development of Finite-Rate Ablation Toolset for Hypersonic Vehicles$140K
- Federal grantDefense · Phase I · Attachment of Additively Manufactured RF Windows for Hypersonics$150K
- Federal grantDefense · Phase I · 3D-Reinforced Melt-Infiltrated Pintle Material$150K
- Federal contractDefense · SBIR Phi$240K
- Federal contractDefense · SIN34 Materials Improvement Program - Task Order 1$587K
- Federal contractDefense · Defense Advanced Research Projects Agency (darpa) Small Business Innovation Research (SBIR) Phase II Effort For Statement Of Work Entitled, "inclusion: Enhanced Ceramic For Improved Thermal Shock Tolerance"$1.2M
- Federal grantDefense · Phase II · Thermal Shock Tolerant Tantalum Carbide Forming MAX Phase Materials$1.5M
- Federal contractDefense · Sbir/sttr Phase II R&d - Thermal Shock Tolerant Tantalum Carbide Forming Max Phase Materials$2.2M
- Federal grantDefense · Phase II · User Element (UEL) Based Process Model for Prediction of C/C Dimensional Changes During Manufacturing$749K
- Federal grantDefense · Phase II · Tape-Wrapped Carbon / Silicon Carbide Composites for Launch Vehicle Applications$750K
- Federal grantDefense · Phase II · High Strain-Rate Characterization Methods for Carbon-Carbon Composites at Elevated Temperature$1.5M
- Federal contractDefense · Sbir/sttr Phase II R&d High Strain-rate Characterization Methods For Carbon-carbon Composites At Elevated Temperature$1.4M
- Federal grantDefense · Phase II · Unit-Cell Approach for C/C Process and Mechanical Modeling$749K
- Federal grantDefense · Phase II · Determination of Carbon-Carbon Hydrocode Parameters by Uncertainty Quantification$1.5M
- Federal contractDefense · Sbir/sttr Phase II R&d, Determination Of Carbon-carbon Hydrocode Parameters By Uncertainty Quantification$1.4M
- Federal contractDefense · Sbir/sttr Phase I Research & Development--tantalum Carbide Forming Max Phase Material For Solid Rocket Motor Throats$150K
- Federal contractDefense · SBIR Phase I Topic A20-027, Title "preliminary Design For Gte Research Grade Cmc Combustor"$111K
- Federal contractDefense · Army Small Business Innovation Research (SBIR) Phase I For Effort Entitled,"development Of Numerical Tool To Optimize The Pyc Fiber Interface Coating In C/sic Composites"$111K
- Federal grantNASA · Phase II · Domestically Available C/C for Hot Structure$750K
- Federal grantDefense · Phase II · Analytical Design of Surface Porosity in 2D C/C to Delay Boundary Layer Transition for Hypersonic Aeroshell Applications$1.5M
- Federal contractDefense · Research And Development$2M
- Federal grantDefense · Phase I · Accelerating the Development of CMAS and Sulfate-Induced Hot Corrosion Resistant Materials through Machine Learning$140K
- Federal grantDefense · Phase I · Preliminary Design for GTE Research Grade CMC Combustor$111K
- Federal grantDefense · Phase I · Development of Numerical Tool to Optimize the PyC Fiber Interface Coating in C/SiC Composites$111K
- Federal grantDefense · Phase I · High Strain-Rate Characterization Methods for Carbon-Carbon Composites at Elevated Temperatures$125K
- Federal contractNASA · Ceramic Matrix Composite (cmc) Testing$339K
- Federal contractDefense · Sbir/sttr Phase I Research&development Determination Of Carbon-carbon Hydrocode Parameters By Uncertainty Quantification$150K
- Federal grantDefense · Phase II · Improved Carbon-Carbon for Hypersonic Vehicles$995K
- Federal contractDefense · SBIR Phase II R&d Improved Carbon-carbon For Hypersonic Vehicles$977K
- Federal grantNASA · Phase I · Rapid Fabrication of CMCs with Aligned Discontinuous Reinforcement via Reactive Melt Infiltration$125K
- Federal contractNASA · Domestically Available C/c For Hot Structure$125K
- Federal contractDefense · TUNNEL9 Throat Assembly$524K
- Federal grantDefense · Phase I · A User Element (UEL) Based Process Model for Prediction of Carbon-Carbon Dimensional Changes During Manufacturing$150K
- Federal contractDefense · Phase 1 - Carbon-carbon Advanced Technologies$150K
- Federal contractDefense · Progress Report$239K
- Federal contractDefense · Small Business Innovative Research Services O182-003-0140 Melt-infiltrated Carbon-carbon Nosetips And Leading Edges For High Velocity, Gun-launched Projectiles$225K
- Federal contractDefense · Throat Assemblies For Aedc$320K
- Federal contractDefense · STTR Phase I Research&development - Uncertainty Reduction In High Speed Flight Vehicle Modeling$100K
- Federal contractDefense · Unit Cell Approach For C/c Process And Mechanical Modeling$150K
- Federal grantDefense · Phase II · Generating Material Properties From Flight Representative Structures$1.5M
- Federal contractDefense · High Temperature Throat Assemblies$325K
- Federal contractDefense · Sbir/sttr Phase II R&d - Development Of Lyocell-based High Temperature Composites For Structural Insulator Applications$994K
- Federal grantDefense · Phase II · Development of Lyocell-Based High Temperature Composites for Structural Insulator Applications$998K
- Federal grantDefense · Phase I · Thin-Ply Composite Missile Structures$100K
- Federal contractDefense · Igf::ot::igf SBIR Phase I Tape-wrapped Carbon/silicon Carbide Composites For Launch Vehicle Applications$150K
- Federal contractDefense · Igf::ot::igf Materials Research And Design Task Order 0003$500K
- Federal contractDefense · Igf::ot::igf Mr&d SBIR III Idiq; To 0002$110K
- Federal grantDefense · Phase II · Ceramic-Metal Joining for Hypersonic Vehicle and Missile Components$1.5M
- Federal grantDefense · Phase I · Load Bearing Thermal Protection Structure for Hypersonic Flight$149K
- Federal contractDefense · Igf::ot::igf Defense Advanced Research Projects Agency (darpa) Small Business Innovation Research (SBIR) Phase I Effort Entitled, "load Bearing Thermal Protection Structure For Hypersonic Flight"$100K
- Federal grantNASA · Phase I · Mechanism Based Damage Model for Linerless Thin-Ply Composite Pressure Vessels$125K
- Federal grantNASA · Phase I · A Mathematical Model to Assess CMAS Damage in EBCs$125K
- Federal contractDefense · Igf::ot::igf Mr&d SBIR III$500K
- Federal grantDefense · Phase I · Rayon Replacement for High Temperature Materials$150K
- Federal contractInterior · Igf::ot::igf Generating Material Properties From Flight Representative Structures$150K
- Federal contractDefense · Igf::ot::igf Materials And Processing For Expendable Hypersonic Vehicles$1.8M
- Federal contractDefense · "igf::ot::igf"$248K
- Federal grantNASA · Phase II · Ceramic Matrix Composite Environmental Barrier Coating Durability Model$750K
- Federal contractNASA · Igf::ot::igf As The Power Density Of Advanced Engines Increases, The Need For New Materials That Are Capable Of Higher Operating Temperatures, Such As Ceramic Matrix Composites (cmcs), Is Critical For Turbine Hot-section Static And Rotating Components. Such Advanced Materials Have Demonstrated The Promise To Significantly Increase The Engine Temperature Capability Relative To Conventional Super Alloy Metallic Blades. They Also Show The Potential To Enable Longer Life, Reduced Emissions, Growth $850K
- Federal contractDefense · Status Report Igf::ot::igf$150K
- Federal grantNASA · Phase I · Fiber Optic Health Monitoring of 3D Woven Preforms and Composites Employing Structurally Integrated Sensors$125K
- Federal contractNASA · Igf::ot::igf Abstract$125K
- Federal contractDefense · Igf::ot::igf SBIR Phase II Research And Development$1.0M
- Federal grantDefense · Phase I · Improved Materials and Designs for High Pressure Wind Tunnel Applications$150K
- Federal contractNASA · Igf::ot::igf As The Power Density Of Advanced Engines Increases, The Need For New Materials That Are Capable Of Higher Operating Temperatures, Such As Ceramic Matrix Composites (cmcs), Is Critical For Turbine Hot-section Static And Rotating Components. Such Advanced Materials Have Demonstrated The Promise To Significantly Increase The Engine Temperature Capability Relative To Conventional Super Alloy Metallic Blades. They Also Show The Potential To Enable Longer Life, Reduced Emissions, Growth M$119K
- Federal contractNASA · Igf::ot::igf To Address The Need For Low-ballistic Coefficient Aeroshells With Minimal Impact On Vehicle Weight, NASA Is Investigating Flexible Thermal Protection System (tps) Options. These Designs Typically Consist Of A Flexible Three-directional (3D) Woven Carbon Cloth That Can Be Stowed During Flight And Deployed On Command To Serve As A Semi-rigid Aeroshell During Atmospheric Entry. For Some Planned Entry Trajectories, The Woven Tps Is Subjected To Short Duration, But Extremely High Heat Fl$125K
- Federal grantDefense · Phase II · Process Optimization of Needled Carbon/ silica carbide (C/SiC) Structural Insulators$1.0M
- Federal contractDefense · Igf::ot::igf Materials Development For Platforms (mdp) Program$4.2M
- Federal grantDefense · Phase II · Innovative Interlaminar Mode I and Mode II Fracture Toughness Test Methods for Ceramic Matrix Composites$500K
- Federal contractDefense · STTR Pii, Materials Research&design, Inc. - Awd$750K
- Federal contractDefense · SBIR Phase I Research&development - "integrated Lightning Strke And Emi Protection Tps Materials For Missile Skin Structures" Igf::ot::igf$125K
- Federal grantDefense · Phase I · Fine Braided Tungsten Reinforced Ceramic Composites for Ultra Sharp Structures$79K
- Federal contractDefense · Igf::ct::igf SBIR 14.2$149K
- Federal grantDefense · Phase II · Manufacturing Process Maturation for Propulsion Technology: Structural Insulators$1.5M
- Federal contractNASA · Igf::ot::igf As The Power Density Of Advanced Engines Increases, The Need For New Materials That Are Capable Of Higher Operating Temperatures, Such As Ceramic Matrix Composites (cmcs), Is Critical For Turbine Hot-section Static And Rotating Components. Such Advanced Materials Have Demonstrated The Promise To Significantly Increase The Engine Temperature Capability Relative To Conventional Super Alloy Metallic Blades. They Also Show The Potential To Enable Longer Life, Reduced Emissions, Growth M$749K
- Federal contractDefense · Igf::ot::igf Sttp 2013-43 Crp Extended Life Mach Throats$1.5M
- Federal contractDefense · N141-082$80K
- Federal contractNASA · Igf::ot::igf The Design Concepts Being Considered For Heatshield For Extreme Entry Environment Technology (heeet) Rely On The Use Of 3D Woven Carbon Fiber Preforms. Therefore, There Is A Need To Be Able To Predict The Properties And Performance Of A Woven Material. Validation Of Predictive Modeling Tools Would Allow For The Use Of These Tools To Design And Optimize The 3D Weaves, Significantly Reducing The Cost Of Fabrication And Testing Of A Variety Of Configurations. While There Are Proven To$750K
- Federal contractDefense · Igf::ot::igf Ph I Research&development. Seek To Reduce The Cost And Delivery Time By Optimizing The Fabrication Parameters. Specifically To Fabricate Billets Of Material Made With Well Planned Variations In A) Interface Coating Thickness, B) Number Of Densification Cycles And C) Maximum Pyrolysis Temperature.$125K
- Federal contractDefense · STTR Phase I$150K
- Federal contractNASA · Igf::ot::igf Based On The Recent Success Of The Mars Exploration Program And The Mars Science Laboratory Mission, NASA Has A Desire To Expand On The Technology Developed Under Each Effort In Order To Increase Future Mission Capabilities, Namely An Increase In Payload Capacity For Entry To Mars, Venus And Other Outer-planets. Such A Goal Requires An Innovative Solution To The Vehicle's Entry, Decent And Landing System (edl). In Order To Address This Goal,nasa Has Recently Invested In The Developm$125K
- Federal contractNASA · Igf::ot::igf As The Power Density Of Advanced Engines Increases, The Need For New Materials That Are Capable Of Higher Operating Temperatures, Such As Ceramic Matrix Composites (cmcs), Is Critical For Turbine Hotsection Static And Rotating Components. Such Advanced Materials Have Demonstrated The Promise To Significantly Increase The Engine Operating Temperature Relative To Conventional Super Alloy Metallic Blades. They Also Show The Potential To Enable Longer Life, Reduced Emissions, Growth Ma$125K
- Federal contractNASA · Igf::ot::igf Current NASA Programs, Such As Adaptable, Deployable Entry And Placement Technology (adept) And Woven Thermal Protection Systems (wtps) Are Looking To Fill A Gap In Ablative Tps For Future Missions To Venus And Saturn, Human Missions Beyond Lunar, And Mars Sample Return Missions. Both Of These Programs Rely On The Use Of 3D Woven Carbon Fiber Preforms. Therefore, There Is A Need To Be Able To Predict The Properties And Performance Of A Woven Material. Validation Of Predictive Modeli$125K
- Federal contractDefense · Igf::cl::igf, DOD 2013.1 SBIR Solicitation$150K
- Federal contractDefense · Igf::cl::igf, Long Range Broad Agency Announcement (baa 13-001) For Navy And Marine Corps Science And Technology$495K
- Federal contractDefense · SBIR Phase III For The Continued Research And Development Required For The Transition Of C-sic Composite Materials Into Navy And Missile Defense Agency Weapon Systems.$4.7M
- Federal contractDefense · SBIR Phase I Topic N121-014 Entitled "low-erosion And Affordable Nozzles For Advanced Air-to-air Missiles"$80K
- Federal contractDefense · R&D$750K
- Federal contractDefense · Research And Development In The Physical, Engineering, And Life Sciences (except Biotechnology)$125K
- Federal contractNASA · Igf::ot::igf Other Functions -- SBIR Phase III -- Evaluation Of Design Concepts And Integrated Materials For Efficient Airframe Structures$24K
- Federal contractNASA · In Order For Carbon-carbon Nozzle Extensions And Exit Cones To Serve As Practical, Low Cost Components For Future Earth-to-orbit Propulsion Systems, It Is Necessary To Develop Alternative Fabrication Methods Coupled With Proven Design And Analysis Tools. Two-dimensional (2D) C-c Components Are Typically Less Expensive And Potentially Lower Weight Than C-c Parts Fabricated Using 3D Woven Preforms. One Typical 2D C-c Fabrication Method Uses A Tape-wrapping Technique In Which A Bias-ply C/ph Tape I$125K
- Federal contractDefense · (STTR Phase 1) Lightweight Composite/hybrid Structures With Enhanced Properties$100K
- Federal contractDefense · Progress Report$80K
- Federal contractDefense · Implication Of Manufactured Delaminations On Cmc$100K
- Federal contractDefense · Basic New Award$750K
- Federal contractNASA · SBIR Phase III -- Jet Test Coupons$10K
- Federal contractNASA · This Project Addresses The Development Of Refractory Coated Or Lined Low Density Structures Applicable For Advanced Future Propulsion System Technologies. The Fundamental Idea Behind This Concept Was To Design A Hot-walled Refractory Material (ceramic And/or Metallic) In The Form Of A Thin Coating Or Liner And Have That Supported By A Low Density Structure Such As Graphite Or Various Carbon-carbon Composites, Offering An Attractive Lightweight Design Option. This Coated Or Lined Low Density Stru$600K
- Federal contractDefense · Research And Development$750K
- Federal contractNASA · As The Operational Demands Of Liquid Rocket Engines Increases, So Too Does The Need For Improved Design And Manufacturing Methods For Metal-to-composite Nozzle Extensions. The State Of The Art Utilizes Non-domestic Composite Materials For Nozzle Extensions. Although This Solution Does Offer Weight Savings And Increased Performance, There Is An Increase In Cost And The Addition Of Export Regulations. Within This Effort, Materials Research&design (mr&d) Is Proposing An Analytical Study, Coupled Wi$100K
- Federal contractNASA · As Space Exploration And Hypersonic Cruise Technologies Develop, The Focus Has Shifted Towards The Development Of Lightweight, Fully Reusable And Lower Cost Vehicles. The Current State-of-the-art (soa) Is Taking An Incremental Improvement Step Over The Space Shuttle Tps Approach. All-ceramic Matrix Composite (cmc) Body Flaps Developed For The X-38 Vehicle Were Shown To Offer Considerable Mass Savings As Well As Increased Durability And Impact Resistance. The Next Step In Advancing The State Of T$100K
- Federal contractDefense · Research And Development In The Physical, Engineering, And Life Sciences (except Biotechnology)$125K
- Federal contractDefense · R&d Under Topic N10B-T050$100K
- Federal contractDefense · Innovative Tps M&p Concepts Development For Structurally Integrated Tps$1.8M
- Federal contractDefense · Conduct Research Into Composite Material That Does Not Degrade During Explosion$70K
- Federal contractDefense · Base Period$409K
- Federal contractDefense · Status Report$140K
- Federal contractDefense · SBIR Phase II Research And Development.$2.2M
- Federal contractNASA · The Innovation In This Proposed Effort Is The Development Of Refractory Coated Or Lined Low Density Structures. Lightweight Structures Are Desirable For Space Transportation Vehicle Systems In Order To Reduce Launch Costs, Increase Mission Flexibility/efficiency, And Add Robustness With Respect To The Ability To Add Weight Or Additional Materials To The Mission With Minimum Sacrifice In Performance. The Use Of Thin Refractory Coatings Over Low Density Structures Will Yield A Lightweight Alternat$100K
- Federal contractNASA · Compared To Superalloys, Ceramic Matrix Composites (cmcs) Offer Reduced Weight And Superior Specific Properties At Elevated Temperatures. However, Cmcs Are Prone To Oxidation Degradation When Exposed To Oxygen At High Temperatures, Which Is The Primary Driver For Useful Life Of The Component. Accurate Predictions Of Cmc Life Require Accurate Predictions Of Oxidation Behavior, Which Require Accurate Values Of The Material Properties That Control The Oxidation Process. One Of These Key Properties $100K
- Federal contractDefense · Research And Development In The Physical, Engineering, And Life Sciences (except Biotechnology)$75K
- Federal contractDefense · Life Prediction Model Incorporating Environmental Effects For S300 Sylramic-ibn/sic Ceramic Matrix Composites$100K
- Federal contractNASA · Mechanical And Thermal Performance Of Cmc Components Benefit From Low Part Count, Integrally Fabricated Designs Of 3D Woven Reinforcement. The Advantages Of These Designs Include The Elimination For The Need For Post-fabrication Mechanical Attachment And The Higher Interlaminar Properties Offered By The Through Thickness Paths Of The Fibers Within The 3D Preform Architectures. The Specific Innovations Mr&d Is Proposing Are To Improve The Preform Geometry Definition Through The Use Of The Kansas $600K
- Federal contractNASA · Materials Research&design (mr&d) Is Proposing In The SBIR Phase II An Effort To Develop A Tool For Predicting The Fatigue Life Of C/sic Composite Laminates, Which Incorporates Mechanical Loading At Any Minimum Stress To Maximum Stress Ratio (i.e., R Value), At Room And Elevated Temperatures, In Either Inert Or Oxidizing Environments. The Success Of This Effort Would Represent A Significant State-of-the-art Improvement In Fatigue Projections Of Ceramic Matrix Composites, Since No Tools Capable Of$600K
- Federal contractDefense · SBIR Pi Topic: N092-115$150K
- Federal contractDefense · Ceramic Matrix Composites$540K
- Federal contractDefense · Research And Development In The Physical, Engineering, And Life Sciences (except Biotechnology)$86K
- Federal contractDefense · Phase II R&d SBIR Topic N07-177$468K
- Federal contractDefense · SBIR Phase I Award$100K
- Federal contractNASA · Calibration Of 3D Woven Preform Design Code For Cmc Materials Future Hypersonic Vehicles Will Utilize Thermal Protection System (tps) Designs And Propulsion System Components That Are Capable Of Experiencing High Temperatures Within Oxidative Environments During Their Operation. These Tps And Propulsion System Components Will Include High Temperature Ceramic Matrix Composites (cmcs), Such As C/sic And Sic/sic. Both Hot Structure Control Surfaces And Hot Wall Propulsion System Components Are Tw$100K
- Federal contractDefense · Research And Development In The Physical, Engineering, And Life Sciences (except Biotechnology)$100K
- Federal contractDefense · Characterization And Modeling Of Pmc/cmc$932K
- Federal contractDefense · Low Cost Fabrication Of Carbon-carbon Aeroshells For Hypersonic Vehicles$750K
- Federal contractFederal Election C · Training$1K
- Federal contractNASA · Multi-axial Damage Index And Accumulation Model For Predicting Fatigue Life Of Cmc Materials$100K
- Federal contractDefense · Phase I SBIR Topic N07-177$147K
- Federal contractNASA · Task 1: Vps Fabrication Of Bulk HFO2 Deposits For Producing Material Property Specimens. Deposits Will Be Sufficient For Producing The Following Specimens. Description Quantity Flexure (0.059" X 0.079" X 0.4-1") 12 Conductivity (0.060" X 0.5-1" Dia.) 2 Cte (0.059" X 0.079" X 0.4-1") 4 TASK2: Scalability Demonstration Of HFO2-IR-RE Fabrication Technique. Goal Is To Develop Vps And El-form Parameters For Producing HFO2-IR-RE Cylinders With An Internal Diameter Greater Than Or Equal To 3.5" L$700K
- Federal contractDefense · SBIR II - Novel High Strenth C-c Nozzle Materials For Advanced Rocket Propulsion$750K
- Federal contractDefense · Lower Cost High Temp Composites$745K
- Federal contractDefense · SBIR Phase II Topic N06-030$996K
- Federal contractDefense · R&d SBIR Phase III Topic N98-149$165K
- Federal contractDefense · Mda SBIR Phase II$991K
- Federal contractDefense · Development Of Non-parasitic Acreage Tps/airframe Material$749K
- Federal contractDefense · Low Cost Fabricatio Of Carbon-carbon (c-c) Aeroshells For Hypersonic Vehicles$100K
- Federal contractNASA · Integrated Durability Model For Ceramic Matrix Composite Components$558K
- Federal contractNASA · SBIR Phase 1 "material Concepts For Light Structure Technology"$100K
- Federal contractNASA · Sap Purchase Requisition: 4200182450 Hypersonic NASA Research Announcement: Design, Fabrication, And Testing Of Load-bearing Thermal Protection Systems (tps)$950K
- Federal contractDefense · 200612!493338!1700!N68335!NAVAL Air Engineering Station !N6833502D0027 !a!n! !Y!0011 ! !20060901!20080303!966563884!966563884!966563884!N!MATERIALS Research & Design IN!300 E Swedesford Rd !wayne !PA!19087!81752!045!42!WAYNE !delaware !penn !+000000374993!N!N!000000000000!AC63!RDTE/ELECTRONICS & Communication Eq-adv Tech Dev !A7 !electronics And Communication Equip !000 !not Discernable !541710!E! !5!B!S! ! ! !999$375K
- Federal contractDefense · 200608!447079!1700!N00178!NAVAL Surface Warfare Center !N0017806C1024 !a!n! !n! ! !20060515!20090531!966563884!966563884!966563884!N!MATERIALS Research & Design IN!300 E Swedesford Rd !wayne !PA!19087!81752!045!42!WAYNE !delaware !penn !+000000050000!N!N!000000669135!AC25!RDTE/MISSILE And Space Systems-eng/manuf Devel !A2 !missile And Space Systems !000 !not Discernable !541330!E! !3! ! ! ! ! !999$918K
- Federal contractDefense · 200608!000700!1700!N65538!NAVAL Sea Logistics Center !N6553806M0185 !a!n! !n! ! !20060510!20070115!966563884!966563884!966563884!N!MATERIALS Research & Design IN!300 E Swedesford Rd !wayne !PA!19087!81752!045!42!WAYNE !delaware !penn !+000000069923!N!N!000000000000!AD91!RDTE/OTHER Defense-basic Research !C9E!ALL Other Supplies And Equipment !000 !not Discernable !541710!E! !9! ! ! ! ! !999$100K
- Federal contractDefense · 200506!154321!1700!N68335!NAVAL Air Engineering Station !N6833505C0168 !a!n! !y! ! !20050315!20070315!966563884!966563884!966563884!N!MATERIALS Research & Design !300 E Swedesford Rd !wayne !PA!19087!81720!005!42!WAYNE (township Of) !armstrong !penn !+000000500000!N!N!000001264467!AC62!RDTE/ELECTRONICS & Communication Eq-applied Resea !A7 !electronics And Communication Equip !000 !* !541710!E! !3! ! ! ! ! !202$1.8M
- Federal contractDefense · 200412!001081!1700!A8050 !naval Air Warfare Center, AIRCRA!N6833502D0027 !a!n! !Y!0009 ! !20040902!20050705!966563884!966563884!966563884!N!MATERIALS Research& Design, IN!300 E Swedesford Road !wayne !PA!19087!81720!005!42!WAYNE (township Of) !armstrong !penn !+000000099075!N!N!000000000000!AC12!RDTE/AIRCRAFT-APPLIED Research !S1 !services !000 !* !541710!E! !5!B!S! ! ! !999$99K
- Federal contractDefense · 200003!1700!000227!A8050 !naval Air Warfare Center, AIRCRA!N6833500C0164 !a!*!* !19991220!20020430!966563884!966563884!966563884!N!067G9!MATERIALS Research& Design, IN!1024 E Lancaster Ave !rosemont !PA!19010!66144!045!42!ROSEMONT !delaware !penn !0001!+000000300000!N!N!000000000000!AC62!RDTE/ELECTRONICS & Communication Eq-applied Resea !A7 !electronics And Communication !2000!NOT Discernable Or Classified !8731!3!*!*!*!B!B!*!A !u!u!$1.8M
Federal awards are summed by year (172 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 84 peers
Line = medianMaterials · Material
- Federal grants#3 · top 4%
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.
Founders appear once a person is matched to the company through its own patents, grants or filings. We never infer people from social profiles.
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
Related companies, and why
- MAINSTREAM ENGINEERING CORPSimilar federal contract value in Materials · $144M in contracts
- MATERIALS SCIENCES LLCSimilar federal contract value in Materials · $119M in contracts
- LUNA LABS USA LLCSimilar federal contract value in Materials · $94.7M in contracts
- MATERIALS ENGINEERING AND TECHNICAL SUPPORT SERVICES CORP.Similar federal contract value in Materials · $66.9M in contracts
- QUESTEK INNOVATIONS LLCSimilar federal contract value in Materials · $62.9M in contracts
- Jimenez Engineering Solutions, LLCSimilar federal contract value in Materials · $55.3M in contracts
Regulatory activity · Materials
- Eliminating Regulations Establishing Fellowships in Laboratory Standardization and Testing for Foreign CitizensNational Institute of Standards and Technology
- Eliminating Obsolete Marking Requirements for Toy, Look-Alike, and Imitation FirearmsNational Institute of Standards and Technology
- Eliminating Obsolete Regulations Related to the Advanced Technology Program and the Technology Innovation ProgramNational Institute of Standards and Technology
Rules are matched to sector, not to company. Recent activity in a sector is context rather than a signal about this business — until rules are matched to what a company actually builds, the section is shown as context and nothing more.
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 .