Federal Contractor Profile
Redwire Space Solutions, LLC
$69M obligated·53 awards·2 agencies·4 NAICS
Federal Contracts
Showing contracts 1–50 of 80 total. Sorted by action date, most recent first. Excludes $0 modifications.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Nov 21, 2024 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $111K |
| Jun 12, 2024 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $100K |
| Jun 28, 2023 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $1.8M |
| May 23, 2023 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $500K |
| Apr 12, 2023 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $111K |
| Feb 16, 2023 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $2.0M |
| Jan 17, 2023 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $2.1M |
| Jul 28, 2022 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $1.9M |
| Jul 13, 2022 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $417K |
| Jun 30, 2022 | Department of DefenseFA9453 AFRL RVK | FA945320C0003 | 541715 | STRUCTURALLY COMBINED APERTURE AND RETICULATED LOCKING EXPANDABLE TRUSS (SCARLET) | $130K |
| May 25, 2022 | Department of DefenseFA9453 AFRL RVK | FA945320C0003 | 541715 | STRUCTURALLY COMBINED APERTURE AND RETICULATED LOCKING EXPANDABLE TRUSS (SCARLET) | $1.2M |
| Feb 23, 2022 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $3.4M |
| Feb 18, 2022 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $750K |
| Jan 19, 2022 | Department of DefenseFA9453 AFRL RVK | FA945320C0003 | 541715 | STRUCTURALLY COMBINED APERTURE AND RETICULATED LOCKING EXPANDABLE TRUSS (SCARLET) | $1.4M |
| Dec 6, 2021 | Department of DefenseFA9453 AFRL RVK | FA945320C0003 | 541715 | STRUCTURALLY COMBINED APERTURE AND RETICULATED LOCKING EXPANDABLE TRUSS (SCARLET) | $1.1M |
| Oct 19, 2021 | Department of DefenseFA9453 AFRL RVK | FA945320C0003 | 541715 | STRUCTURALLY COMBINED APERTURE AND RETICULATED LOCKING EXPANDABLE TRUSS (SCARLET) | $610K |
| Oct 5, 2021 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $3.1M |
| Aug 16, 2021 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC21P2416 | 541330 | ENGINEERING CONSULTING | $82K |
| Jun 21, 2021 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $73K |
| Jun 21, 2021 | National Aeronautics and Space AdministrationNASA MARSHALL SPACE FLIGHT CENTER | 80MSFC21CA008 | 541715 | SOLAR CRUISER: SOLAR SAIL SYSTEM (SSS) AND ACTIVE MASS TRANSLATOR (AMT) | $2.5M |
| Jun 16, 2021 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC21C0047 | 541715 | SOLAR CRUISER | $602K |
| Apr 8, 2021 | Department of DefenseFA9453 AFRL RVK | FA945320C0003 | 541715 | STRUCTURALLY COMBINED APERTURE AND RETICULATED LOCKING EXPANDABLE TRUSS (SCARLET) | $250K |
| Feb 18, 2021 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC21C0047 | 541715 | SOLAR CRUISER | $604K |
| Aug 28, 2020 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865020C9216 | 541715 | LUNAR ARTICULATING SOLAR PANEL SYSTEM | $1.5M |
| Jul 14, 2020 | Department of DefenseFA9453 AFRL RVK | FA945320C0003 | 541715 | STRUCTURALLY COMBINED APERTURE AND RETICULATED LOCKING EXPANDABLE TRUSS (SCARLET) | $4.9M |
| May 19, 2020 | Department of DefenseFA8808 MIL SATELLITE COM SYS PKT LA | FA880820C0019 | 541715 | ARTICULATED TENSIONED HEXAPOD EXTENDABLE NANOSATELLITE ANTENNA(ATHENA) | $799K |
| Apr 15, 2020 | Department of DefenseFA8808 MIL SATELLITE COM SYS PKT LA | FA880820C0019 | 541715 | ARTICULATED TENSIONED HEXAPOD EXTENDABLE NANOSATELLITE ANTENNA(ATHENA) | $1.5M |
| Mar 6, 2020 | Department of DefenseFA8649 USAF SBIR STTR CNTRCTNG AFRL | FA864920P0948 | 541715 | COMPACT HIGH ENERGY STORAGE SYSTEM | $50K |
| Dec 23, 2019 | Department of DefenseFA9453 AFRL RVK | FA945320C0017 | 541715 | EXPERIMENT FOR LONG LIFE INNOVATIVE ENERGY | $10M |
| Dec 18, 2019 | Department of DefenseFA9453 AFRL RVK | FA945320C0003 | 541715 | STRUCTURALLY COMBINED APERTURE AND RETICULATED LOCKING EXPANDABLE TRUSS (SCARLET) | $1000K |
| Dec 13, 2019 | Department of DefenseFA9453 AFRL RVK | FA945317C0426 | 541712 | IGF::OT::IGF DEPLOYABLE STRUCTURAL BOOMS FOR SMALLSAT ANTENNAS | $4.0M |
| Nov 6, 2019 | Department of DefenseFA8808 MIL SATELLITE COM SYS PKT LA | FA880820C0019 | 541715 | ARTICULATED TENSIONED HEXAPOD EXTENDABLE NANOSATELLITE ANTENNA(ATHENA) | $751K |
| Sep 5, 2019 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833519C0517 | 541715 | RESEARCH AND DEVELOPMENT | $749K |
| Aug 13, 2019 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC19C0127 | 541715 | ARTICULATING SOLAR PANEL ENERGY SYSTEM (ASPEN) | $749K |
| Aug 5, 2019 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC19C0513 | 541715 | SAIL TRIMMING ACTUATOR FOR TARGETED REENTRY (STARTR) | $125K |
| Aug 2, 2019 | Department of DefenseFA8649 USAF SBIR STTR CNTRCTNG AFRL | FA864919PA303 | 541715 | ARTICULATED TENSIONED HEXAPOD EXTENDIBLE NANOSATELLITE ANTENNA (ATHENA) | $50K |
| Jul 30, 2019 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC19C0469 | 541715 | SPACE DEMONSTRATION OF FLEXCOOL THIN FLAT HEAT PIPES | $125K |
| Jul 24, 2019 | Department of DefenseFA9453 AFRL RVK | FA945319P0673 | 541715 | HIGH POWER RADIATOR AND SWITCHABLE ADVANCED THERMAL SYSTEMS | $150K |
| May 16, 2019 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865019C9228 | 541715 | ROBUST, HIGHLY SCALABLE SOLAR ARRAY FOR HARSH ENVIRONMENTS | $1.5M |
| Feb 28, 2019 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014716C7726 | 541712 | IGF::OT::IGF SBIR PHASE II RESEARCH&DEVELOPMENT | $500K |
| Feb 27, 2019 | Department of DefenseFA8650 USAF AFMC AFRL PZL AFRL/PZL | FA865019C9202 | 541715 | ROBUST, HIGHLY SCALABLE SOLAR ARRAY FOR HARSH ENVIRONMENT | $1.5M |
| Dec 17, 2018 | Department of DefenseFA9453 AFRL RVK | FA945319P0542 | 336419 | IGF::OT::IGF STANDARDIZED SCALABLE COMPONENTS FOR ESPA-CLASS POWER SYSTEMS | $150K |
| Dec 6, 2018 | Department of DefenseFA9453 AFRL RVK | FA945319C0597 | 541715 | SHEAR STABILIZATION BASED FRAMEWORK FOR THE FAILURE TESTING AND ANALYSIS OF HSCS | $750K |
| Nov 28, 2018 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014719C7040 | 541715 | SBIR/STTR PHASE I RESEARCH&DEVELOPMENT - SYSTEM FOR ULTRAHIGH RATE AND GRAVIMETRICALLY EFFICIENT STORAGE | $99K |
| Aug 23, 2018 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014715C7215 | 541712 | 7215 PHASE II R&D IGF::OT::IGF FOR OTHER FUNCTIONS | $499K |
| Aug 8, 2018 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833518C0117 | 541715 | IGF::OT::IGF | $100K |
| Jul 20, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P1969 | 541715 | IN RESPONSE TO NASA S NEED FOR A COMPACT, LOW-COST AND AUTONOMOUS DEPLOYABLE SOLAR ARRAY SYSTEM TO SUPPORT MARTIAN SURFACE EXPLORATION, ROCCOR PROPOSES TO ENHANCE THE MARS COMPACT TELESCOPING SURFACE ARRAY (CTSA) BASELINE DESIGN BY INCORPORATING AN ARTICULATING SOLAR PANEL ENERGY SYSTEM (ASPEN). THE MARS CTSA WAS ESTABLISHED IN 2017 AS THE CULMINATION OF AN EXTENSIVE TRADE PERFORMED AT NASA S LANGLEY RESEARCH CENTER WITH THE GOAL TO SUPPORT HUMAN MARS EXPLORATION. THE ASPEN SYSTEM INCLUDES PV CELLS BONDED TO A THIN MEMBRANE THAT IS Z-FOLDED WHILE STOWED, AND PULLED OUT / TENSIONED WHEN DEPLOYED. THE ASPEN SYSTEM REPLACES TRADITIONAL MEMBRANE PV BLANKETS WITH LIGHTWEIGHT PANELS THAT CAN BE ARTICULATED IN UNISON MUCH LIKE VENETIAN BLINDS. THIS PRESENCE OF ARTICULATION AND RESULTING GAPS BETWEEN SUBSTRATES OFFER UNIQUE ADVANTAGES FOR OPERATION ON THE MARTIAN SURFACE: 1) REDUCED CELL DENSITY LEADING TO INCREASED PERFORMANCE IN COST, W/KG AND KW/M3, 2) IMPLEMENTATION OF ARRAY POROSITY AND ARTICULATION CONTROL TO REDUCE INTERACTION WITH MARTIAN WIND AND MITIGATE DUST COLLECTION, AND 3) MODULAR DESIGN THAT ENABLES MASS PRODUCTION AND EASE OF REPLACEMENT. | $123K |
| Jul 20, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P2161 | 541715 | TO ENABLE THE USE OF KILOWATT CLASS FISSION POWER SYSTEMS FOR SURFACE MISSIONS TO THE MOON AND MARS ROCCOR PROPOSES THE DEVELOPMENT OF A FLAT, TITANIUM/WATER HEAT PIPE WITH AN INTEGRATED DEPLOYABLE COMPOSITE RADIATOR. THE PROPOSED DESIGN LEVERAGES ROCCOR S EXPERIENCE IN HIGH STRAIN COMPOSITE DEPLOYABLE STRUCTURES AND TWO-PHASE THERMAL MANAGEMENT PRODUCTS FOR SPACECRAFT APPLICATIONS. HEAT PIPES CURRENTLY PROVIDE A HIGHLY CONDUCTIVE PASSIVE HEAT TRANSFER SOLUTION, BUT TRADITIONAL HEAT PIPES ARE CUMBERSOME TO INTERFACE TO THE STIRLING ENGINE AND RADIATOR PANELS AND DIFFICULT TO BEND TO PROPER CONFIGURATIONS. WHILE THE CURRENT STATE-OF-ART IS ABLE TO HANDLE THE HEAT LOAD, NASA HAS IDENTIFIED DEPLOYABILITY AND THERMAL INTERFACES AS FOCUS AREAS FOR FUTURE THERMAL RADIATORS. ROCCOR PROPOSES TO UTILIZE THEIR FLEXCOOL THIN FLAT HEAT PIPES COUPLED WITH ROCOOL FLEXIBLE CONDUCTIVE MATERIALS (K>1,000 W/M-K), AND WITH ENOUGH STRAIN ENERGY TO PASSIVELY DEPLOY A NOVEL INTEGRATED KILOPOWER RADIATOR. ROCCOR S THIN, FLAT FLEXCOOL HEAT PIPES CAN INTERFACE TO FLAT SURFACE WITH LOW THERMAL RESISTANCE, PROVIDE IMPROVED RADIATOR FIN EFFICIENCY, AND ARE SIMPLE TO BEND. FLEXCOOL WILL ALSO BE COUPLED WITH ROCOOL HIGHLY CONDUCTIVE (K>1,000 W/M-K) FLEXIBLE BLANKET MATERIALS THAT USES PROPRIETARY PROCESSES TO LAMINATE PYROLYTIC GRAPHITE INTO A COMPOSITE RADIATOR MATERIAL THE OVERARCHING PHASE I OBJECTIVE IS TO DEMONSTRATE THE TECHNICAL FEASIBILITY OF THE PROPOSED HEAT PIPE/RADIATOR, AND CONDUCT A PRELIMINARY DESIGN-ANALYSIS-FABRICATION LOOP FOR A 200-WATT PANEL CAPABLE OF MEETING THE REQUIREMENTS FOR SUNPOWER S CURRENT 80W STIRLING ENGINE TECHNOLOGY. THE MATURATION OF THIS TECHNOLOGY WOULD ENABLE THE USE OF FISSION POWER SYSTEMS LARGER THAN 1 KWE WHICH WOULD ENHANCE CURRENT MISSION CAPABILITIES. | $122K |
| Jul 20, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P2199 | 541715 | IN RESPONSE TO NASA S NEED FOR LONG-DURATION, LOW-MASS IN-SPACE MODULAR CONSTRUCTION COMPONENTS, ROCCOR PROPOSES TO DEVELOP STRUCTURAL JOINTS DESIGNED FOR RAPID IN-SPACE ASSEMBLY (ISA) AND STRUCTURAL MODULARITY. TRUSSES BUILT OF REPEATING UNIT-CELL/MODULAR ELEMENTS CAN BE ASSEMBLED BY CONNECTING MULTIPLE MODULES TO INTERCONNECTING JOINTS. IMPLEMENTED WITH EMBEDDED CONDUCTORS FOR CONNECTION VERIFICATION, POWER AND DATA TRANSMISSION, THE PROPOSED INVENTION UTILIZES NEAR ZERO CTE COMPOSITE TUBES WITH SNAP-FIT CONNECTORS AND A FLEXIBLE JOINT FOR QUICK, REPEATABLE CONSTRUCTION AND RECONFIGURATION OF TRUSSES IN SPACE. THE CONCENPT, FLEXIBLE I NTERCONNECTING NODES FOR IN-SPACE STRUCTURAL ASSEMBLY (FINESS), WILL ADVANCE ISA OPPORTUNITIES THROUGH INNOVATIVE FEATURES SUCH AS: 1) ASSEMBLY CONNECTIONS AT LOW-WEIGHT, LOW COST, AND MINIMAL PART-COUNT, 2) DEVELOPING RIGID PLUG-AND-PLAY JOINTS FOR CONNECTING MODULES IN VARIOUS ARRANGEMENTS, 3) INTEGRATING CONDUCTIVE ELEMENTS FOR A FULLY CONNECTED STRUCTURE WITH JOINT CONNECTION VERIFICATION, AND 4) NEAR ZERO THERMAL EXPANSION IN CARBON FIBER TUBES AND CONNECTING FIXTURES. THE PRINCIPAL OBJECTIVE FOR THE PHASE I PROJECT IS TO CONDUCT A PRELIMINARY DESIGN-ANALYSIS-FABRICATION-TEST LOOP FOR AN ELECTRICALLY INTEGRATED MODULAR TRUSS JOINT. THE PROJECT WILL CLEARLY IDENTIFY ENGINEERING RISKS THAT MUST BE ADDRESSED TO ENSURE ACCEPTABLE PERFORMANCE ON-ORBIT AND IN GRAVITY LOADED ENVIRONMENTS. DETAILED MECHANICAL AND ELECTRICAL DESIGN WILL BE PERFORMED INCLUDING INVESTIGATION OF ATTAINABLE TRUSS GEOMETRIES, REPEATABLE PLUGAND- PLAY FASTENING MECHANISMS, MATERIAL SELECTION AND CONDUCTIVE ROUTING. THE DESIGN EFFORTS WILL BE FOLLOWED BY LOCAL AND GLOBAL STRENGTH, STABILITY AND THERMAL ANALYSES TO DESCRIBE THE CAPACITY OF THE MODULAR JOINTS. FURTHERMORE, ELEMENTS OF THE CONCEPT WILL BE PROTOTYPED TO TEST AREAS SUCH AS MODULAR ASSEMBLY AND ELECTRICAL CONTINUITY ACROSS JOINTS. | $124K |
| Jul 18, 2018 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | 80NSSC18P2116 | 541715 | THIS BODY OF RESEARCH FOCUSES ON DEVELOPING FUNDAMENTAL ENGINEERING QUALIFICATION METHODS FOR THIN-PLY HIGH STRAIN COMPOSITES (TPHSCS). ROCCOR WILL COLLABORATE WITH NASA AND DR. KWOK OF THE UNIVERSITY OF CENTRAL FLORIDA TO DEVELOP AND VALIDATE A ROBUST FRAMEWORK FOR ENGINEERING THE VISCOELASTIC BEHAVIOR OF HIGHLY STRAINED THIN-PLY COMPOSITES. THE MATERIAL SYSTEMS STUDIED WILL BE HIGHLY FOCUSED ON THE MATRIX CONTRIBUTIONS TO THIN PLY COMPOSITE STRUCTURES, WHERE THE FIBERS UTILIZED WILL BE IM7 AND THE LAYUP TYPE WILL BE SPREAD-TOW PLAIN WEAVE WITH A MAXIMUM OF 80 GRAMS PER SQUARE METER. THE ULTIMATE GOAL OF THIS RESEARCH IS TO DEVELOP A ROBUST ANALYSIS AND PREDICTION METHOD WHICH IS MATRIX AGNOSTIC, HOWEVER WITH THE TIMEFRAME OF A PHASE ONE CONTRACT THE INITIAL STUDY WILL ONLY UTILIZE PATZ MATERIALS TECHNOLOGIES F7 (PMT-F7) TOUGHENED, HIGH TEMPERATURE, EPOXY RESIN. PERFORMANCE TASKS OF THIS PROGRAM INCLUDE NEAT-RESIN TEST, COLUMN-BEND TEST, AND DIAMETRICAL COMPRESSION TESTING. EACH TEST WILL AID IN THE DEVELOPMENT OF ROBUST ANALYTICAL METHODS AS WELL AS MATERIAL ALLOWABLE DATABASES MADE AVAILABLE TO THE PUBLIC. FURTHER INVESTIGATION IN A PHASE TWO EFFORT WOULD VALIDATE THE FRAMEWORK AND PUBLISH TEST DATA FOR A REPRESENTATIVE SAMPLE OF SPACE-FLIGHT-GRADE RESIN TYPES INCLUDING AT LEAST ONE OTHER EPOXY, CYANATE ESTER, THERMOPLASTIC (E.G. PEEK, PEKK), AND AT LEAST ONE SYSTEM WITH A NANO-FILLER. | $125K |
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