Contractor directory

PEREGRINE FALCON CORP

PLEASANTON, CA · UEI LXQQB47E1RA3 · CAGE 084E5

Largest contract awards

• 80NSSC21C0007$3.6M

  CONSOLIDATION OF HEAT PIPES WITHIN A U-8MO CORE FOR HIGH EFFICIENCY AND LONG-TERM RELIABILITY. THERMAL ENERGY CONVERSION. LIQUID INTERFACE DIFFUSION BONDING OF FPS HEAT PIPES TO CORE

  National Aeronautics and Space Administration · NAICS 541715 · Dec 2020 – Dec 2022 · official record ↗

• HQ086021C7152$2.7M

  SBIR/STTR PHASE II R&D

  Missile Defense Agency · NAICS 541715 · May 2021 – Jun 2026 · official record ↗

• SP470123C0063$2.0M

  SBIR PHASE II PROPOSAL #L2-0413 TENDERED UNDER TOPIC # DLA22.2-007 FOR CONVERSION COATED SURFACES FOR HYPERSONIC ENVIRONMENTS PHASE II PROPOSAL.

  Defense Logistics Agency · NAICS 541715 · Sep 2023 – Sep 2025 · official record ↗

• N6833521C0232$1.9M

  RESEARCH AND DEVELOPMENT

  Department of the Navy · NAICS 541715 · Feb 2021 – Jul 2026 · official record ↗

• N0002424CS053$1.7M

  BASE

  Department of the Navy · NAICS 541715 · Apr 2024 – Apr 2027 · official record ↗

• HQ014717C7409$1.7M

  ::IGF::OT::IGF SBIR/STTR PHASE II R&D

  Missile Defense Agency · NAICS 541712 · Jun 2017 – Oct 2021 · official record ↗

• FA239423CB058$1.2M

  CONVERSION COATINGS FOR HIGH TEMPERATURE PROTECTION OF NIOBIUM ALLOYS

  Department of the Air Force · NAICS 541715 · Aug 2023 – Feb 2025 · official record ↗

• NNX16CC19C$897K

  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 POINTED TO THE SINK OF SPACE. THE CURRENT STATE OF THE ART DESIGNS DO NOT MEET THIS REQUIREMENT AND RELY UPON HEAT PIPES TO AXIALLY CARRY THE WASTE THERMAL LOADS WHILE RADIATING FINS, WITH TYPICAL THERMAL GRADIENTS AND LOSSES, PROVIDE THERMAL DISTRIBUTION AWAY FROM THE HEAT PIPES VIA SIMPLE CONDUCTION. UNDER PHASE I, PEREGRINE HAS SUCCESSFULLY DEMONSTRATED AN ALTERNATIVE DESIGN WHICH PROMISES TO BE LOWER IN MASS WHILE IMPROVING PERFORMANCE BASED UPON PULSATING HEAT PIPES (PHPS). PHPS CAN DIRECTLY ACQUIRE AND THEN READILY DISTRIBUTE THERMAL LOADS ACROSS THE FACE OF RADIATOR PANELS TO CREATE HIGHLY EFFICIENT NEAR ISOTHERMAL DESIGNS. PHPS ARE AN AUTONOMOUS, SELF-CONTAINED, LOW PROFILE, LIGHTWEIGHT, HIGH PERFORMANCE THERMAL TRANSPORT SYSTEM BASED UPON HEAT OF VAPORIZATION. PHASE II WILL CHARACTERIZE A TITANIUM/WATER PULSATING HEAT PIPE SYSTEM, BUILD PROTOTYPES OF A PULSATING HEAT PIPE (PHP) RADIATOR FOR A 1 KWE FPS, AND ALSO BUILD A CONVENTIONAL HEAT PIPE DESIGN IN ORDER TO PROVIDE A SIDE BY SIDE COMPARISON OF PERFORMANCE INCREASES OF PHPS VERSUS THE CONVENTIONAL DESIGN. PHASE II WILL PROVIDE OBJECTIVE DATA THROUGH EMPIRICAL RESULTS FOR FUTURE EFFICIENT LIGHTWEIGHT, ISOTHERMAL RADIATOR DESIGNS.

  National Aeronautics and Space Administration · NAICS 541712 · Apr 2016 – Nov 2019 · official record ↗

• NNX17CC06C$744K

  IGF::OT::IGF A KEY CHALLENGE TO PRODUCING 10KWE FISSION POWER SYSTEMS (FPS) IS EMBEDDING AND JOINING HEAT PIPES INTERNALLY TO THE U-7MO CORE. A SUCCESSFUL PHASE I EFFORT HAS DEMONSTRATED THE FEASIBILITY OF APPLYING THE TECHNOLOGY OF LIQUID INTERFACE DIFFUSION (LID) BONDING TO EMBED AND JOIN HEAT PIPES (HAYNES 230) TO THE CORE. AN ADDED BONUS IS THAT THIS LID BONDING TECHNOLOGY WILL SIMULTANEOUSLY ELIMINATE THE SEAMS AND VOIDS CREATED FROM A CORE MADE FROM PIECES OF U-7MO THEREBY PROVIDING AN INTEGRATED HEAT PIPE / U-7MO CORE SUB-ASSEMBLY WITH NO INTERNAL VOIDS OR SEPARATIONS BETWEEN CORE PIECES OR FROM THE CORE TO THE HEAT PIPES. LID BONDING WILL EVEN ALLOW FOR THE CORE TO BE BUILT UP BY VARIOUS HORIZONTAL AND ASYMMETRIC PIECES SUCH AS SPLIT HEAT PIPE CHANNELS TO EASILY RECEIVE HEAT PIPES, CONSOLIDATING THE CORE MATERIAL AROUND THE HEAT PIPES DURING THE LID BONDING PROCESS. PHASE II WILL ALLOW NASA TO PRODUCE FPS UP TO 10 KWE AND BEYOND TO MEET THE POWER REQUIREMENTS FOR LANDING ASTRONAUTS ON MARS, AND ALSO TO PROVIDE POWER TO A HOST OF OTHER PROGRAMS, INCLUDING PROGRAMS SUCH AS NEPTUNE SYSTEMS EXPLORER, KUIPER BELT OPTIC, TROJAN TOUR, AND JUPITER EUROPA ORBITER.

  National Aeronautics and Space Administration · NAICS 541712 · May 2017 – Nov 2019 · official record ↗

• SP470124C0058$732K

  LOW COST MULTI-LAYER METAL INSULATION AS A HYPERSONIC AEROSTRUCTURE WITH THERMAL PROTECTION SYSTEMS R&D SUPPORT SERVICES

  Defense Logistics Agency · NAICS 541715 · Aug 2024 – Aug 2026 · official record ↗

• W15QKN17C0115$664K

  IGF::OT::IGF PHASE III SBIR NOVEL MMIC HIGH FLUX HEAT EXCHANGER:2 WATT THERMAL

  Department of the Army · NAICS 541712 · Sep 2017 – Dec 2019 · official record ↗

• N6833522C0625$239K

  SBIR PHASE I

  Department of the Navy · NAICS 541715 · Aug 2022 – Nov 2023 · official record ↗

Public records from FPDS (via USAspending.gov) and SAM.gov. Figures reflect harvested award data and may not be complete; verify against the linked official records. Not an endorsement. Company in the data by mistake or wish to update it? Email support@usegovscout.com.