Peregrine Falcon Corporation
Conversion coatings (carburizing and anodizing surface treatments) for refractory metals (tungsten, niobium, hafnium) to protect hypersonic vehicles
- Sector
- Aerospace
- Headquarters
- Pleasanton, CA
- Total capital
- $21.6M
- Federal grants
- $13.3M
- 18 awards · 2016–2026
- Rank in peer group#10 of 61
- Private capital raised
- None on recordNo Form D filings on SEC EDGAR. Some raises are not filed.
- Federal contracts
- $8.3M
- 24 awards · Defense, NASA
- Rank in Aerospace#261 of 1335
- Granted patents
- 3
- first 2023
- Rank in peer group#13 of 61
Capital timeline
Latest events
- Federal grantDefense · Phase I · STTR Phase I Topic DLA25D-003 Peregrine Falcon Corp, "heat Pipe Solutions For Nose Tips And Leading Edges"$99K
- Federal grantDefense · Phase II · Low Cost Multi-layer Metal Insulation As A Hypersonic Aerostructure With Thermal Protection Systems R&d Support Services$644K
- Federal grantDefense · Phase II · BASE$1.2M
- Federal grantDefense · Phase I · STTR Phase I Topic A23B-T005 For Joining Of Ultra-high Temperature Ceramics (uhtcs) To Substrate For Ultra-high Temperature Performance.$197K
- Federal grantDefense · Phase II · DLA222-007-0130 Conversion Coated Surfaces for Hypersonic Environments PHASE II Proposal$998K
- Federal grantDefense · Phase II · Conversion Coatings for High Temperature Protection of Niobium Alloys$1.2M
- Federal grantDefense · Phase I · Low Cost MLMI as a Hypersonic Aerostructure with TPS$99K
Show 35 earlier federal awards
- Federal contractDefense · Peregrine Falcon SBIR Phase I Proposal L23A-003-0025 Award SP4701-23-P-0065$98K
- Federal grantDefense · Phase I · Conversion Coated Surfaces for Hypersonic Environments$100K
- Federal grantDefense · Phase I · High Temperature Fin and Control Surfaces$239K
- Federal grantDefense · Phase II · MDA15-020 MLMI Forward Conical Section of an Interceptor Body for Hypersonic Defense Systems$2.7M
- Federal grantNASA · Phase II · Consolidation of Heat Pipes within a U-8Mo Core for High Efficiency and Long-Term Reliability$3.6M
- Federal contractDefense · Progress Report$238K
- Federal grantNASA · Phase I · Lunar Lander - Autonomous Variable Radiator$125K
- Federal grantNASA · Phase I · Multi-Layer Metal Insulation with Aerostructure for Hot Structure$125K
- Federal grantDefense · Phase I · Improved Seals for Hypersonic Vehicles$150K
- Federal contractNASA · Peregrine Has Successfully Developed An Innovative Technology Under The Phase II SBIR Effort. This Phase Ii-e Effort Will Utilize The Developments To Date And Extend The Research To Further Light-weight And Increased Performance Of Isothermal Radiators Produced From Titanium With Embedded Flat Heat Pipes Filled With A Working Fluid Of Water (a Proven Long Life System). In Phase II, Peregrine Demonstrated The Ability To Produce 1 Meter Size Functioning Radiators That Are Near Isothermal In Their $176K
- Federal grantDefense · Phase I · Advanced Machining of Aerospace Materials$150K
- Federal contractDefense · SBIR Phase I-peregrine Falcon Corporation- R&d For Lightweight Structures For Future Interceptors (B181-006-0134)$99K
- Federal contractNASA · Multi-layer Insulation (mli) Package$63K
- Federal contractDefense · Igf::ot::igf Phase III SBIR Novel Mmic High Flux Heat EXCHANGER:2 Watt Thermal$664K
- Federal contractDefense · ::igf::ot::igf Sbir/sttr Phase II R&d$1.7M
- Federal grantNASA · Phase I · Advanced Athermal Telescopes$124K
- Federal grantNASA · Phase II · Liquid Interface Diffusion Bonding of FPS Heat Pipes to Core$744K
- Federal contractNASA · Igf::ot::igf Peregrine Proposes The Combination And Use Of Of BE-38AL, Electroless Nickel Plating, And Single Point Diamond Turning To Create Precision X-ray Grazing Optical Surfaces. Large X-ray Telescopes Will Demand Large, High Stiffness, And Lightweight Substrates To Provide Rigidity To Support The Production Of Nested Optical Surfaces While Requiring Accurate Alignment Through The Use Of Stable Support Structures. Ideally, These Nested X-ray Mirrors Would Be Of Heavy Metal, Microns In Thic$125K
- Federal contractNASA · Igf::ot::igf Peregrine Proposes The Development Of ?liquid Interface Diffusion? (lid) Bonding To Be The Joining Method To Provide A Homogeneous Connection Between The Heat Pipes And Cores Of Fission Power Systems (fps). This Innovation Will Create A High Strength, High Temperature And High Integrity (homogeneous) Joint Between The Hanes 230 Alloy Comprising The Nak Heat Pipe Wall And U-8MO Core. This Homogeneous Joint Will Allow For High Efficiency Heat Transfer From The Core To Nak Heat Pipes W$124K
- Federal contractNASA · Igf::ot::igf Peregrine Will Develop A Multi-layer Radiation Shield (mlrs) That Will Provide The Equivalent Insulation Of A 30 Layer 1.25? Thick Mli Blanket In The Vacuum Of Space But On The Surface Of Mars. Mlrs Will Provide Superior Properties To Mli But In A Much Smaller Profile, Mlrs Can Be Accurately Modeled And Simulated So It Is Predictable, It Can Be Pre-qualified, Provide Higher Performance With No Outgassing, And, When Placed Onto The Exteriors Of Systems, Can Provide Micrometeorite Pro$125K
- Federal grantNASA · Phase II · Pulsating Heat Pipes$747K
- Federal contractNASA · Igf::ot::igf Large Radiator Panels, Based Upon State Of The Art Conventional Heat Pipes With Attached Fins For Thermal Load Distribution And Dissipation Is The Current Baseline Design For Nasa?s Fission Power System. The Initial 1 Kwe Fps Requires A Total Radiating Surface Of 2.5 M2. Higher Power Designs Will Require Corresponding Larger Radiating Surfaces. In Order To Achieve Optimum Radiator Performance, The Face Sheets Of These Radiators Should Present Waste Heat Loads As Isothermal Sheets P$897K
- Federal contractDefense · Igf::ot::igf SBIR Phase I Research And Development$134K
- Federal contractNASA · Igf::ot::igf An Advanced Heat Transport Technology Is Presented That Can Enable Space Nuclear Power Systems To Transfer Reactor Heat, Convert Heat Into Electricity, Reject Waste Heat, And Provide High Thermal Conductivity To Enhance Waste Heat Transfer And Radiator Performance. This Is A Low Cost, Autonomous, High Reliability And Long-life Solution. This Technology Can Operate At High Temperatures Up To 1,000 K To Either Provide Heat Transport For Reactor Cooling Or To Dramatically Increase Ther$125K
- Federal contractNASA · Igf::ot::igf Peregrine Will Bring Together Recent Laboratory Developments And Mature The Technology So That Complete Mirror And Telescope Assemblies Can Be Reliably And Robustly Produced. This Proposed Innovation Will Lower The Cost Of Space Mirrors From Their Current State Of The Art Of $6.4 M/M2 To Less Than $1.6 M/M2 While Maintaining Low Weight, High Stiffness And High Performance For X-ray, Neutron And Uv/optical Mirrors. The Basis Of This Approach Relies Upon BE-38AL (a Lower Cost Berylliu$749K
- Federal contractNASA · Igf::ot::igf Peregrine Will Bring Together Recent Laboratory Developments And Mature The Technology So That Complete Mirror And Telescope Assemblies Can Be Reliably And Robustly Produced. This Proposed Innovation Will Lower The Cost Of Space Mirrors From Their Current State Of The Art Of $6.4 M/M2 To Less Than $1.6 M/M2 While Maintaining Low Weight, High Stiffness And High Performance For X-ray, Neutron And Uv/optical Mirrors.$125K
- Federal contractDefense · Igf::ot::igf Ph I Research&development: Lightweight Optical Benches And Moutning Structures$99K
- Federal contractDefense · Igf::ot::igf Ph I Research&development Title: Mw Class Hel High Altitude Cooling System$125K
- Federal contractDefense · Igf::ot::igf Ph II SBIR: Novel Monolithic Microwave Integrated Circuit (mmic) High Flux Heat.$1.2M
- Federal contractDefense · Phase I SBIR - Novel Monolithic Integrated Circuit (mmic) High Flux Heat Exchanger$149K
- Federal contractDefense · Mda SBIR Phase 1$90K
- Federal contractNASA · Thermal Pyrolytic Graphite Enhanced Components Peregrines Innovation Will Reduce The Required Input Power, Increase A Coolers Systems Margin For A Giving Cooling Load And Reduce Vibration Accordingly For Cryocoolers. Our Innovation Will Enhance The Thermal Conductivities Of Structures Associated With The Cryocooler, Enable Much More Efficient Heat Removal And Thereby Produce A More Efficient System. Effectively We Will Be Increasing The Thermal Conductivities Of The Structures Associated With T$490K
- Federal contractDefense · SBIR Phase 1, Topic #N08-128$80K
- Federal contractNASA · Thermal Pyrolytic Graphite Enhanced Components$99K
- Federal contractDefense · Mda SBIR Phase II$568K
Federal awards are summed by year (42 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 61 peers
Line = medianAerospace · Material
- Federal grants#10 · top 16%
- Granted patents#13 · top 21%
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
USPTO · 3 granted of 3- GrantedMulti-layer Metal Insulation To Shunt Thermal Transfer From External Environments Above 1200 Degrees CelsiusUSPTOUS 12,275,214
- GrantedSolid State Diffusion Bonding Of Refractory Metals And Their AlloysUSPTOUS 11,833,606
- GrantedSolid State Diffusion Bonding Of Refractory Metals And Their AlloysUSPTOUS 11,654,504
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- HINETICS LLCSimilar federal contract value in Aerospace · $8M in contracts
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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
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 .