Federal Contractor Profile
Deep Space Systems INC
$49M obligated·28 awards·2 agencies·8 NAICS
Federal Contracts
Showing award actions 101–127 of 127 funded award actions, most recent first.
- Contracts with positive obligations
- 28
- Funded award actions shown
- 127
- Obligations shown
- $49M
- Awarding agencies
- 2
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 June 23, 2026. Source: USAspending federal award records.
| Date | Agency | PIID | NAICS | Description | Amount |
|---|---|---|---|---|---|
| Dec 13, 2017 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $366K |
| Nov 21, 2017 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $255K |
| Nov 16, 2017 | Department of DefenseNAVAIR WARFARE CTR AIRCRAFT DIV | N6833518C0116 | 541715 | IGF::OT::IGF | $125K |
| Nov 8, 2017 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $37K |
| Nov 6, 2017 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014718C7220 | 541715 | IGF::OT::IGF SBIR/STTR PHASE I RESEARCH&DEVELOPMENT,PROPOSAL NUMBER: B172-006-0218, PROPOSAL TITLE: LOADPATH ENHANCED GIMBAL SYSTEM | $100K |
| Aug 29, 2017 | Department of DefenseFA9453 AFRL RVK | FA945312C0070 | 541712 | THERMAL CONTROL FOR OPERATIONALLY RESPONSIVE SPACE (ORS) SATELLITES | $37K |
| Jul 21, 2017 | Department of DefenseFA9453 AFRL RVK | FA945312C0070 | 541712 | THERMAL CONTROL FOR OPERATIONALLY RESPONSIVE SPACE (ORS) SATELLITES | $199K |
| Jun 26, 2017 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014717C7407 | 541712 | ::IGF::OT::IGF SBIR/STTR PHASE II R&D | $1000K |
| Jun 9, 2017 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $129K |
| Jun 5, 2017 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX17CL74P | 541712 | IGF::OT::IGF FOR MARS MISSION PROGRAM MANAGERS, WHO NEED A ROBUST, STRUCTURALLY EFFICIENT SOLAR ARRAY SYSTEM TO AUTONOMOUSLY DEPLOY ON THE MARTIAN SURFACE, THE MODULAR EXTENDABLE TERRESTRIAL ARRAY (META) IS AN EXTREMELY HIGH PERFORMANCE AND COST-EFFECTIVE DEPLOYABLE SOLAR ARRAY SYSTEM THAT WILL ENABLE MANNED MISSIONS. LOADPATH'S APPROACH ADAPTS A DEMONSTRATED, HIGH PACKAGING-EFFICIENCY ARRAY FOLDING ARCHITECTURE FOR A MARTIAN SURFACE APPLICATION DELIVERING ROBUST AUTONOMOUS DEPLOYMENTS OVER UNEVEN TERRAIN, RETRACTABILITY, MODULARITY, PORTABILITY, MINIMAL CONOPS, AND INTEGRATED DUST MITIGATION. LOADPATH RECENTLY INVENTED AND DEMONSTRATED THE FEASIBILITY OF AN ADVANCED, LIGHTWEIGHT SOLAR ARRAY SYSTEM TO DELIVER HIGH POWER GENERATION CAPABILITY FOR SMALL SATELLITE SYSTEMS WITH EXTREME STOWED VOLUME CONSTRAINTS. ESTABLISHING A FUNCTIONAL SOLAR ARRAY FARM ON THE MARTIAN SURFACE TO SUPPORT MANNED MISSIONS SHARES MANY OF THE TECHNICAL CHALLENGES AND REQUIREMENTS OF THE SMALL SPACECRAFT, LARGE DEPLOYABLE ARRAY PROBLEM. LOADPATH LEVERAGED THE FINDINGS OF THIS PREVIOUS EFFORT WITH ITS EXTENSIVE EXPERIENCE IN DEVISING AND DELIVERING NUMEROUS INNOVATIVE DEPLOYABLE STRUCTURAL SYSTEMS IN THE DEVELOPMENT OF THE LEADING CONCEPT FOR AN META AUTONOMOUS DEPLOYING TERRESTRIAL ARRAY. IN THIS PHASE I EFFORT, THE CONCEPTUAL DESIGN WILL BE DEVELOPED THROUGH A THOROUGH ENGINEERING TRADE STUDY OF THE REQUIRED SUPPORT COMPONENTS, CULMINATING WITH A FUNCTIONAL DEPLOYMENT DEMONSTRATION WITH A FABRICATED PROTOTYPE STRUCTURE. | $125K |
| Apr 20, 2017 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $46K |
| Apr 12, 2017 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $52K |
| Jan 10, 2017 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $150K |
| Dec 1, 2016 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $80K |
| Nov 10, 2016 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $80K |
| Oct 20, 2016 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $66K |
| Aug 4, 2016 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $250K |
| Jun 17, 2016 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014716C7528 | 541712 | IGF::OT::IGF SBIR PHASE I RESEARCH AND DEVELOPMENT | $40K |
| Jun 6, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX16CM16P | 541712 | IGF::OT::IGF FOR SMALL SATELLITE PROGRAM MANAGERS AND INTEGRATORS, WHO MUST CONTEND WITH INCREASING POWER CONSUMPTION OF SMALL SPACECRAFT WITH ADVANCED ELECTRIC PROPULSION AND/OR SCIENCE INSTRUMENTATION, THE STRUCTURAL ORIGAMI ARRAY (SOAR) IS AN EXTREMELY HIGH PERFORMANCE DEPLOYABLE SOLAR ARRAY SYSTEM THAT DELIVERS 200W TO 1KW+ POWER OUTPUT, WHILE EXCEEDING STATE-OF-THE-ART PACKAGING EFFICIENCIES. UNLIKE EXISTING FOLDING PANEL OR ROLLED ARCHITECTURES, OUR APPROACH UTILIZES A SIMPLE RELIABLE DEPLOYABLE SUPPORTING STRUCTURE AND A TWO-DIMENSIONAL ORIGAMI PACKAGING SCHEME OF THE FLEXIBLE BLANKET/SUBSTRATE THAT EXHIBITS SEVERAL UNIQUE AND ENABLING CHARACTERISTICS. THESE INCLUDE A PERFECT PACKAGING EFFICIENCY, EQUAL TO Z-FOLDING; SMALL STOWED SQUARE FORM FACTOR TO EASILY FIT INTO ANY SMALL SATELLITE; EASILY SCALABLE TO CREATE LONGER ARRAYS WITH LITTLE IMPACT ON STOWED HEIGHT, COMPLEXITY, AND STRUCTURAL PERFORMANCE; UNIFORM FOLDING MECHANICS FOR SIMPLE ELECTRONIC HARNESSING; DETERMINISTIC FOLDING KINEMATICS THAT UNFOLD IN TWO DIMENSIONS WHEN PULLED ALONG ITS LENGTH, WHICH MINIMIZES POTENTIAL ARRAY DAMAGE DURING DEPLOYMENT; AND AN INHERENT THICKNESS INSENSITIVITY, WHICH ALLOWS FOR THE USES OF THICKER, LONG LIFESPAN OR HIGH EFFICIENCY PHOTOVOLTAIC CELLS. | $125K |
| May 17, 2016 | Department of DefenseFA9453 AFRL RVK | FA945312C0070 | 541712 | THERMAL CONTROL FOR OPERATIONALLY RESPONSIVE SPACE (ORS) SATELLITES | $230K |
| Apr 28, 2016 | National Aeronautics and Space AdministrationNASA SHARED SERVICES CENTER | NNX14CJ04C | 541712 | IGF::OT::IGF FOR SPACECRAFT DESIGN AND DEVELOPMENT TEAMS CONCERNED WITH COST AND SCHEDULE, THE QUICK SPACECRAFT THERMAL ANALYSIS TOOL (QUICKSTAT) IS AN INNOVATIVE SOFTWARE SUITE THAT WILL SIGNIFICANTLY REDUCE LABOR COSTS AND EFFORT ASSOCIATED WITH THE DESIGN, ANALYSIS, AND OPTIMIZATION OF SPACECRAFT. UNLIKE TRADITIONAL ANALYSIS WHERE HIGHLY-TRAINED ENGINEERS SPEND DAYS TO MONTHS DEVELOPING, RUNNING, AND EVALUATING HIGH-RESOLUTION MODELS, QUICKSTAT PROVIDES THE SIMILAR RESULTS IN NEAR REAL-TIME TO A BROADER RANGE OF USERS. QUICKSTAT WILL ENABLE, ON ONE HAND, HIGHLY SKILLED THERMAL ENGINEERS TO MORE EFFECTIVELY EXPLORE COMPLEX DESIGN SPACES, WHILE ON THE OTHER HAND GIVE BETTER ENGINEERING DESIGN ACCESS TO LESS SKILLED ENGINEERS AND PROGRAM STAKEHOLDERS. FOR THERMAL ANALYSTS INVOLVED IN MULTI-DIMENSIONAL TRADE STUDIES, QUICKSTAT PROVIDES THE MEANS TO RAPIDLY COMPARE HUNDREDS OR THOUSANDS OF DISCRETE DESIGN POINTS AND IDENTIFY TRENDS THAT LEAD TO MORE OPTIMAL DESIGN SOLUTIONS. FOR DESIGNERS OF LOW-COST SPACECRAFT, QUICKSTAT CAN ENABLE QUICK AND EFFICIENT THERMAL DESIGN TRADE STUDIES WITHOUT INVESTING IN A HIGH-END THERMAL ANALYSIS TOOLS. | $125K |
| Mar 9, 2016 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $270K |
| Mar 1, 2016 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $147K |
| Feb 16, 2016 | Department of DefenseFA9453 AFRL RVK | FA945312C0070 | 541712 | THERMAL CONTROL FOR OPERATIONALLY RESPONSIVE SPACE (ORS) SATELLITES | $532K |
| Jan 14, 2016 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $103K |
| Dec 30, 2015 | Department of DefenseFA9453 AFRL RVK | FA945311C0265 | 541712 | BAA VS-07-03 CALL 0020 - INTEGRATED DESIGN ANALYSIS&TESTING OF SPACE STRUCTURES | $132K |
| Dec 18, 2015 | Department of DefenseMISSILE DEFENSE AGENCY (MDA) | HQ014716C7528 | 541712 | IGF::OT::IGF SBIR PHASE I RESEARCH AND DEVELOPMENT | $100K |
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