Redwire Space Technologies, INC.

$67M obligated·74 awards·3 agencies·6 NAICS

Federal Contracts

Showing award actions 201–210 of 210 funded award actions, most recent first.

Contracts with positive obligations: 74
Funded award actions shown: 210
Obligations shown: $67M
Awarding agencies: 3

This table shows award actions with a positive obligation. Zero-dollar and negative-dollar actions, such as administrative changes and deobligations, are not displayed. Multiple award actions may belong to the same contract.

Award data as of August 6, 2026. Source: USAspending federal award records.

Date	Agency	PIID	NAICS	Description	Amount
Jun 9, 2017	National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER	NNX17CA55P	541712	IGF::OT::IGF ACCORDING TO THE DECADAL REPORT TITLED, LIFE AND PHYSICAL SCIENCES RESEARCH FOR A NEW ERA OF SPACE EXPLORATION, A REPORT, ??THE AHB PANEL WOULD BE REMISS IF IT DID NOT STRONGLY RECOMMEND AN ANIMAL CENTRIFUGE CAPABLE OF ACCOMMODATING RATS/MICE AT VARIABLE GRAVITY LEVELS.? FURTHERMORE, THE PANEL STATED, ??RESEARCH ON ANIMAL MODELS WILL BE CONSTRAINED WITHOUT THE ABILITY TO MANIPULATE THE GRAVITY VARIABLE AS A FACTOR MODULATING THE FUNDAMENTAL PROCESSES UNDERLYING ORGAN SYSTEM HOMEOSTASIS.? IN RESPONSE, TECHSHOT HAS PROPOSED TO DEVELOP A RODENT CENTRIFUGE FACILITY (RCF-QL) THAT UTILIZES FOUR LOCKER LOCATIONS (QUAD LOCKER) IN THE EXPRESS RACK FOR LIFE SCIENCE RESEARCH. THE COUNTER-BALANCED CENTRIFUGE IS DESIGNED TO PROVIDE A FACILITY TO ALLOW RATS AND MICE TO LIVE AND BE OBSERVED IN SIMULATED GRAVITY BETWEEN 0-1 G FOR UP TO 90 DAYS. THE RCF-QL PROVIDES UP TO FIVE CAGES. EACH CAGE CAN ACCOMMODATE AT LEAST SIX 30 GRAM MICE, THREE 200 GRAM RATS, OR TWO 400 GRAM RATS PER CAGE. EACH INDIVIDUAL CAGE HAS ABLIB FOOD AND WATER, CONTROLLABLE LIGHTING, AND VIDEO MONITORING. THE HABITAT IS TEMPERATURE CONTROLLED WITH CONSTANT AIRFLOW THROUGHOUT THE CAGES. AIR FLOW ENTRAPS WASTE IN A FILTER THAT ALSO TREATS THE WASTE FOR BACTERIA AND ODOR. ADDITIONAL AIR FILTERS WILL REMOVE ODORS AND AMMONIUM FROM THE ANIMAL ENCLOSURE. THE SUBSYSTEMS DESIGN WILL MINIMIZE CREW TIME. EACH SUBSYSTEM REQUIRING CHANGE-OUT DURING THE 90 DAY EXPERIMENT WILL BE DESIGNED TO BE SIMPLE AND INTUITIVE IN OPERATIONS. THE RCF-QL WILL BE THE ONLY FACILITY CAPABLE OF PROVIDING GROUP HOUSING FOR RATS AND MICE, WITH A MEDIUM DIAMETER CENTRIFUGE (20 IN., 0.508 M) AND A LARGE ROTATING CAGE VOLUME (1000 IN3, 16,400 CM3 FOR THE CAGE). ALL HARDWARE CAGE FEATURES ARE DESIGNED TO MEET NIH ANIMAL CARE AND USE STANDARDS.	$125K
Apr 24, 2017	National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER	NNX17CM03C	541712	IGF::OT::IGF TECHSHOT'S INNOVATIVE 3D METAL PRINTER OFFERS THE UNIQUE ABILITY TO FABRICATE METAL COMPONENTS AND TOOLS IN SPACE WHICH CAN BE UTILIZED FOR SUSTAINABILITY, MAINTENANCE AND RESEARCH. THE PROPOSED SYSTEM WILL ACCOMPLISH THIS TASK THROUGH THE UTILIZATION OF A TWOSTAGE FILAMENT MELTING PROCESS WHEREBY A METALLIC FILAMENT IS FIRST HEATED TO CURIE TEMPERATURE THROUGH INDUCTION AND THEN DEPOSITED ON A BUILD PLATFORM WHERE IT IS FUSED TO THE PREVIOUS LAYER BY EXPOSURE TO A LOW ENERGY LASER. THIS NEW UNIQUE PROCESS IS KNOWN AS SINTERED METAL PRINTING WITH LASER EXPOSURE (SIMPLE). INDUCTION HEATING IS NOT ENTIRELY NEW TO FUSED DEPOSITION MANUFACTURING (FDM). THERE HAS BEEN RECENT RESEARCH INTO THE INTEGRATION OF AN INDUCTION COIL INTO THE "HOT END" OF A PLASTIC FILAMENT FDM PRINTER. THE INDUCTION COIL SURROUNDS THE METAL NOZZLE, KNOWN AS THE "HOT END" AND INDUCTIVELY HEATS THE NOZZLE WHEN AN AC CURRENT IS APPLIED. THE NOZZLE THEN HEATS AND MELTS THE PLASTIC FILAMENT ALLOWING IT TO BE EXTRUDED ONTO A PLATFORM WHERE A PART IS FORMED. THE USE OF INDUCTION HEATING, WHEN PRINTING WITH A METAL FILAMENT, IS SIMILAR BUT THE INDUCTION COIL HEATS THE WIRE FILAMENT DIRECTLY AS IT PASSES THROUGH ITS CENTER. THIS SYSTEM OFFERS FASTER MELT TIMES RESULTING IN FASTER FEED RATES, LOWER MASS RESULTING IN QUICKER MORE ACCURATE PRINTER HEAD MOVEMENTS AND LOWER OVERALL POWER CONSUMPTION. CONCEPTUALLY, THE WIRE FILAMENT WILL NOT BE HEATED TO MELTING BUT HEATED TO THE CURIE TEMPERATURE AND LAID AS A HOT FILAMENT ON THE BUILD PLATFORM. TO GAIN ADHERENCE BETWEEN DEPOSITED LAYERS, A LOW ENERGY LASER IS USED SIMULTANEOUS TO THE LAYERING PROCESS TO HEAT AND FUSE ADJACENT FILAMENT LAYERS.	$750K
Apr 14, 2017	National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER	NNJ17GU32T	541712	IGF::OT::IGF MICRO13	$1.4M
Jan 23, 2017	National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER	NNJ17GU14T	541712	IGF::OT::IGF PASSIVE ORBITAL NUTRIENT DELIVERY SYSTEM, PONDS, THIS TASK ORDER IS TO COMPLETE THE REQUIREMENTS NECESSARY FOR AN ENHANCED PASSIVE WATER DELIVERY SYSTEM, EPWDS, TO BE USED TO GROW PLANTS IN THE VEGETABLE PRODUCTION, VEGGIE FACILITIES ON THE INTERNATIONAL SPACE STATION AND IN GROUND FACILITIES AT KENNEDY SPACE CENTER, KSC. THE EPWDS WILL BE DESIGNED TO PROVIDE MORE RELIABLE WATER AND NUTRIENT DELIVERY TO PLANTS IN MICROGRAVITY. A GOVERNMENT- DEVELOPED EPWDS PROTOTYPE CALLED PASSIVE ORBITAL NUTRIENT DELIVERY SYSTEM, PONDS WILL BE USED FOR THE DESIGN, DEVELOPMENT, AND TESTING OF THE SPACE-FLIGHT QUALIFIED HARDWARE. TECHSHOT WILL WORK WITH A COMMERCIAL ENTITY TO DEVELOP THE HARDWARE. THE FOLLOWING TASKS WILL BE COMPLETED FOR THIS PROJECT.	$484K
Jan 10, 2017	National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER	NNJ17GU15T	541712	IGF::OT::IGF THE BD MEASURES X-RAY ABSORPTION BY BONE AND SOFT TISSUE AND REPORTS BONE DENSITY IN MICE. IT CAN ALSO DETERMINE SOFT-TISSUE DENSITY, LEAN/FAT RATIO AND TOTAL ANIMAL MASS (I.E., WEIGHING MICE IN SPACE). THE BO FLIGHT UNIT WAS DEVELOPED AND MANUFACTURED TO OPERATE SAFELY ON THE INTERNATIONAL SPACE STATION {ISS), WHERE IT CURRENTLY RESIDES FOR USE IN THE NATIONAL LABORATORY. THE BD TECHNOLOGY PROVIDES BONE MINERAL AND BODY COMPOSITION RESULTS FROM TOTAL BODY IMAGING IN LESS THAN 5 MINUTES. FAST IMAGING ALLOWS FASTER ACCESS TO IMPORTANT DATA AND IS SAFE FOR THE ANIMALS.	$35K
Sep 14, 2016	National Aeronautics and Space AdministrationNASA JOHNSON SPACE CENTER	NNJ16GU25T	541712	IGF::OT::IGF BONE SCANNING SERVICES TO SUPPORT RODENT RESEARCH-5 PER THE ATTACHED STATEMENT OF WORK.	$276K
Jun 29, 2016	Department of DefenseW4PZ USA MED RSCH ACQUIS ACT	W81XWH15C0005	541712	IGF::OT::IGF SBIR PHASE III ARMY, ERMS# 14245004, DEVELOP ASES PROTOTYPE	$140K
Jun 3, 2016	National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER	NNX16CM34P	541712	IGF::OT::IGF THE PROPOSED INNOVATION IS A 3D METAL PRINTER, WHICH OFFERS THE UNIQUE ABILITY TO FABRICATE METAL COMPONENTS AND TOOLS IN SPACE. THE PROPOSED SYSTEM WILL ACCOMPLISH THIS TASK THROUGH THE UTILIZATION OF A TWO-STAGE FILAMENT MELTING PROCESS WHEREBY A METALLIC FILAMENT IS FIRST HEATED TO CURIE TEMPERATURE THROUGH INDUCTION AND THEN DEPOSITED ON A BUILD PLATFORM WHERE IT IS FUSED TO THE PREVIOUS LAYER BY EXPOSURE TO A LOW ENERGY LASER. THIS NEW UNIQUE PROCESS IS KNOWN AS SINTERED METAL PRINTING WITH LASER EXPOSURE (SIMPLE). INDUCTION HEATING IS NOT ENTIRELY NEW TO FUSED DEPOSITION MANUFACTURING (FDM). THERE HAS BEEN RECENT RESEARCH INTO THE INTEGRATION OF AN INDUCTION COIL INTO THE "HOT END" OF A PLASTIC FILAMENT FDM PRINTER. THE INDUCTION COIL SURROUNDS THE METAL NOZZLE, KNOWN AS THE "HOT END" AND INDUCTIVELY HEATS THE NOZZLE WHEN AN AC CURRENT IS APPLIED. THE NOZZLE THEN HEATS AND MELTS THE PLASTIC FILAMENT ALLOWING IT TO BE EXTRUDED ONTO A PLATFORM WHERE A PART IS FORMED. THE USE OF INDUCTION HEATING, WHEN PRINTING WITH A METAL FILAMENT, IS SIMILAR BUT THE INDUCTION COIL HEATS THE WIRE FILAMENT DIRECTLY AS IT PASSES THROUGH ITS CENTER. THIS SYSTEM OFFERS FASTER MELT TIMES RESULTING IN FASTER FEED RATES, LOWER MASS RESULTING IN QUICKER MORE ACCURATE PRINTER HEAD MOVEMENTS AND LOWER OVERALL POWER CONSUMPTION. CONCEPTUALLY, THE WIRE FILAMENT WILL NOT BE HEATED TO MELTING BUT HEATED TO THE CURIE TEMPERATURE AND LAID AS A HOT FILAMENT ON THE BUILD PLATFORM. TO GAIN ADHERENCE BETWEEN DEPOSITED LAYERS, A LOW ENERGY LASER IS USED SIMULTANEOUS TO THE LAYERING PROCESS TO HEAT AND FUSE ADJACENT FILAMENT LAYERS.	$125K
May 6, 2016	National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER	NNX16CJ16C	541712	IGF::OT::IGF FROZEN TISSUE SAMPLES REPRESENT THE STATE OF THE ART IN TISSUE PRESERVATION IN MANY MOLECULAR ANALYSIS TECHNIQUES AS WELL AS IN IN MEMBRANE ANALYSIS USING FREEFRACTURE TECHNIQUES. RAPID FREEZING ELIMINATES THE ARTIFACT CAUSED BY ICE CRYSTAL FORMATION WITHIN THE TISSUES. ICE CRYSTAL NUCLEATION AND GROWTH OCCURS BETWEEN 0? C AND -20?C TYPICALLY. TO AVOID THIS DAMAGE AND MINIMIZE DESTRUCTION OF PROTEINS, RNA AND DNA BY LYTIC ENZYMES, CELLS OR TISSUES HAVE TO BE RAPIDLY COOLED THROUGH THIS TEMPERATURE BAND. THIS IS TYPICALLY DONE IN AN ISOPENTANE BATH COOLED BY LIQUID NITROGEN (LN2) TO -150?C. THIS 2 STEP PROCESS ELIMINATES ARTIFACTS CAUSED BY ICE NUCLEATION AS WELL AS ARTIFACTS CAUSED BY NITROGEN BUBBLES THAT SURROUND THE TISSUE AS IT BOILS IF SUBMERGED DIRECTLY INTO LN2. WHILE THESE OPEN METHODS ARE ACCEPTABLE FOR TERRESTRIAL LABORATORIES, THEY WOULD NOT BE COMPATIBLE WITH EXPERIMENTATION ON THE INTERNATIONAL SPACE STATION. OUR PROPOSED GASEOUS NITROGEN-BASED RAPID FREEZER CLAMP WOULD PROVIDE AN ALTERNATIVE MEANS TO RAPID COOL THROUGH ICE CRYSTAL NUCLEATION AND GROWTH TEMPERATURES WITHOUT EXPOSING THE CREW TO THE SPILL HAZARDS OF LN2 AND CHILLED ISOPENTANE AS WELL AS THE EXTREME FLAMMABILITY OF ISOPENTANE.	$750K
Feb 4, 2016	Department of DefenseW4PZ USA MED RSCH ACQUIS ACT	W81XWH16C0019	541711	DHP SBIR PH II #H2-0119. IGF::OT::IGF	$1000K

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