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Federal Contract Awards

17awards

Analyze awards, watch incumbents and competitors, track new transactions or changes, and use award history to shape recompete and capture strategy.

Awardee
is
QLJLWGE4MHD4
Award ID
Description
Recipient
Total Value
Awarding Agency
Funding Agency
Set Aside
NAICS
PSC
Award Date
Start Date
End Date
W911RQ24C0005
ROADWHEEL ADHESIVE APPLICATION SYSTEM SERVICE SUPPORTACCUDYNE SYSTEMS, INC.$236,062DEPT OF THE ARMYDEPT OF THE ARMY—541512Computer Systems Design ServicesR425SUPPORT- PROFESSIONAL: ENGINEERING/TECHNICALMar 28, 2024Mar 28, 2024Oct 31, 2024
W911RQ22C0008
MANUFACTURE AND PROVIDE A COMPLETE TURNKEY ROADWHEEL AUTOMATED ADHESIVE SPRAY SYSTEM.ACCUDYNE SYSTEMS, INC.$3,882,000DEPT OF THE ARMYDEPT OF THE ARMY—3332493620RUBBER AND PLASTICS WORKING MACHINERYSep 14, 2022Sep 14, 2022Nov 25, 2024
W9132T22P0030
HYDROTHERMAL LIQUIFICATION SYSTEM FOR HAB MITIGATION U435CFMACCUDYNE SYSTEMS, INC.$778,900DEPT OF THE ARMYUS ARMY CORPS OF ENGINEERS - CIVIL PROGRAM FINANCING ONLY—334513Instruments and Related Products Manufacturing for Measuring, Displaying, and Controlling Industrial Process Variables4410INDUSTRIAL BOILERSJul 7, 2022Jul 7, 2022Mar 31, 2023
NNX17EC72P
SAP PURCHASE REQUISITION: 4200619047 IGF::OT::IGF TROUBLESHOOT AEROGEL DRYING MACHINE. PROVIDE AND INSTALL TRIM KIT AND HIGH CAPACITY FILTER.ACCUDYNE SYSTEMS, INC.$5,633NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—333249J034MAINT/REPAIR/REBUILD OF EQUIPMENT- METALWORKING MACHINERYApr 18, 2017Apr 18, 2017May 18, 2017
NNC12VD94P
CHAMBER UPGRADEACCUDYNE SYSTEMS, INC.$37,758NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—333298K059MODIFICATION OF EQUIPMENT- ELECTRICAL AND ELECTRONIC EQUIPMENT COMPONENTSMay 1, 2012May 1, 2012Sep 15, 2012
FA865011M5186
AUTOMATION OF MATERIAL PLACEMENT FOR AIRCRAFT RADOMESACCUDYNE SYSTEMS, INC.$142,883DEPT OF THE AIR FORCEDEPT OF THE AIR FORCE—541711AD91Sep 29, 2011Sep 27, 2011Jun 27, 2012
N6833510C0116
R&D SBIR PHASE II TOPIC N08-026ACCUDYNE SYSTEMS, INC.$1,087,162DEFENSE CONTRACT MANAGEMENT AGENCY (DCMA)DEPT OF THE NAVY—541712AC62Jul 20, 2010Jul 20, 2010Oct 15, 2015
NNX09CB71C
WHILE IN THE 1970'S AND 1980'S, COMPOSITES WERE ADOPTED FOR AEROSPACE STRUCTURE FOR INCREASED PERFORMANCE AND WEIGHT SAVINGS, THE 1990'S AND 2000'S WITNESSED THE ATTENTION TOWARDS COST-EFFECTIVE FABRICATION. ALL THERMOSET PROCESSES THAT UTILIZE SUCH MACHINES RELY ON AUTOCLAVES TO CONSOLIDATE THE LAMINATES, AT SIGNIFICANT ACQUISITION AND OPERATIONAL EXPENSE. AUTOCLAVES TO CONSOLIDATE WINGS ARE HUGELY EXPENSIVE. AUTOCLAVES FOR FUSELAGES ARE NEARLY COST-PROHIBITIVE (ONLY ONE EXISTS). AUTOCLAVES FOR THE ARES V DO NOT EXIST. THE MARKETPLACE WOULD WELCOME A PROVEN OUT-OF-AUTOCLAVE FABRICATION TECHNOLOGY. THE TASKS IN THE ASI/UD-CCM STTR PHASE 1 WAS TO ASSESS THE PERFORMANCE OF THE CURRENT TP-ATP HEADS, DO A MODEL BASED PARAMETRIC STUDY TO DETERMINE POSSIBLE HEAD AND PROCESS PARAMETER CHANGES AND DEMONSTRATE AN IMPROVED UNDERSTANDING OF THE HEAD, WITH A GOAL OF AUTOCLAVE LEVEL PROPERTIES. A SET OF MODELS FOR THE IN SITU AUTOMATED TOW/TAPE PLACEMENT (ATP) PROCESSES THAT CAPTURE THE IMPORTANT PROCESS PHENOMENA WERE DEVELOPED BY UD-CCM. ACCUDYNE THEN MEASURED THE LAMINATE ROUGHNESS, FABRICATED SAMPLES USING A VARIETY OF CONDITIONS AND TESTED THE SAMPLES. TESTING OF THE LAMINATES INDICATE: PLACING WITH FLAT TAPE AND USING IMPROVED HEAD CHILLING INCREASES MECHANICAL PROPERTIES. COMPACTING WITH ONLY A LOAD REDUCES PROPERTIES. USING A VACUUM BAG OVEN RECONSOLIDATION IS INEFFECTIVE, AND EVEN REDUCES MECHANICAL PROPERTIES. THE PHASE 2 PROGRAM INNOVATION IS TO DEVELOP AND DEPLOY UNIVERSITY OF DELAWARE PROCESS MODELS TO ACCUDYNE'S THERMOPLASTIC TOW AND TAPE PLACEMENT HEAD TO REMEDY THE MECHANICAL PROPERTY SHORTFALL BETWEEN THE TWO FABRICATION PROCESSES USED TO MANUFACTURE LARGE COMPOSITE AEROSPACE STRUCTURE IMPORTANT TO NASA. AN ADDITIONAL ADVANTAGE THAT WOULD ACCRUE BY ADOPTING TP-ATP WOULD BE THE USE OF NOVEL THERMOPLASTIC MATERIALS WITH THERMAL STABILITY AND TOUGHNESS FAR IN EXCESS OF WHAT THERMOSETTING MATERIALS CAN ACHIEVE.ACCUDYNE SYSTEMS, INC.$599,487NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHJun 22, 2009Jun 22, 2009Sep 30, 2011
N6833508C0499
FINAL REPORT SBIR TOPIC N08-135ACCUDYNE SYSTEMS, INC.$149,898DEPT OF THE NAVYDEPT OF THE NAVY—541712AC61Sep 15, 2008Sep 15, 2008Mar 14, 2009
N6833508C0195
R & D SBIR PHASE I TOPIC N08-026ACCUDYNE SYSTEMS, INC.$67,823DEPT OF THE NAVYDEPT OF THE NAVY—541712AC61Mar 27, 2008Mar 27, 2008Sep 24, 2008
NNX08CD45P
OUT-OF-AUTOCLAVE THERMOPLASTIC TAPE/TOW PLACEMENT (TP-ATP) IS NEARING COMMERCIALIZATION BUT SUFFERS A MODERATE GAP IN MECHANICAL PROPERTIES COMPARED WITH LAMINATES FABRICATED VIA THERMOSET AUTOCLAVE PROCESSING. OUT-OF-AUTOCLAVE THERMOPLASTIC PROCESSING SIGNIFICANTLY LOWERS COMPOSITE AEROSPACE PART COSTS BUT THE PROPERTY GAP MUST BE CLOSED. THIS STTR PROGRAM ENDORSED HEREIN BY BOEING AND CYTEC ENGINEERED MATERIALS WILL REMEDY THE MECHANICAL PROPERTY SHORTFALL AND ENABLE LARGE COMPOSITE AEROSPACE STRUCTURE IMPORTANT TO NASA TO BE MANUFACTURED WITHOUT AN AUTOCLAVE. ACCUDYNE IS TEAMING WITH UNIVERSITY OF DELAWARE A CENTER FOR COMPOSITE MATERIALS TO APPLY THEIR STATE-OF-THE-ART TP-ATP PROCESS/PROPERTY MODELS TO ELUCIDATE THE PHYSICAL MECHANISMS AFFECTING MICROSTRUCTURAL QUALITY THAT CAUSE THE PROPERTY GAP. MODELS WILL BE APPLIED TO THE NASA LARC TP-ATP DEPOSITION HEAD TO OPTIMIZE THE HEAD CONFIGURATION AND MACHINE OPERATING PARAMETERS AND THE CONTROL SYSTEMS FOR FULL MECHANICAL PROPERTIES. LAMINATES WILL BE MANUFACTURED TO DEMONSTRATE THE PROPERTY IMPROVEMENTS. THE PROCESS HEAD AND EQUIPMENT CHANGES WILL BE UPGRADED ON THE NASA-LARC THERMOPLASTIC TAPE HEAD. IN PHASE 2 PROCESS/HEAD MODELING WILL BE EXTENDED THROUGH LAMINATE FABRICATION AND TESTING AND A COMPONENT OF INTEREST TO NASA WILL BE FABRICATED DEMONSTRATING THE IMPROVED AUTOCLAVE LEVEL MECHANICAL PERFORMANCE.ACCUDYNE SYSTEMS, INC.$99,935NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONNATIONAL AERONAUTICS AND SPACE ADMINISTRATION—541712AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHJan 25, 2008Jan 25, 2008Jan 16, 2009
FA930006MT017
200610!000256!5700!FA9300!AFFTC/PKT !FA930006MT017 !A!N! !Y! ! !20060720!20070108!960998474!960998474!960998474!N!ACCUDYNE SYSTEMS INC !134 SANDY DR !NEWARK !DE!19713!50670!003!10!NEWARK !NEW CASTLE !DELAWARE !+000000050000!N!N!000000000000!AC21!RDTE/MISSILE AND SPACE SYSTEMS-BASIC RESEARCH !A2 !MISSILE AND SPACE SYSTEMS !000 !NOT DISCERNABLE !541710!E! !9! ! ! ! ! !99990909!C! ! !A! !D!U!J!1!001! ! !Z!N!Z! ! !N!B!N!N! ! !Z! !A!A!000!A!B!N! ! ! ! ! ! !0001! !ACCUDYNE SYSTEMS, INC.$0DEPT OF THE AIR FORCEDEPT OF THE AIR FORCE—541710AC21NATIONAL DEFENSE R&D SERVICES; ATOMIC ENERGY DEFENSE ACTIVITIES; BASIC RESEARCHJul 20, 2006Jul 20, 2006Feb 4, 2007
NNL05AA89P
SBIR I -- OPTIMAL COMPOSITE MATERIALS USING NASA RESINS OR POSS NANO PARTICLE MODIFICATIONS FOR LOW COST FABRICATION OF LARGE COMPOSITE AEROSPACE STRUCTURESACCUDYNE SYSTEMS, INC.$68,204NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541710AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHJan 21, 2005Jan 21, 2005Jul 25, 2005
NNL05AA05C
SBIR PHASE II-HEATED THERMOPLASTIC FIBER PLACEMENT HEADACCUDYNE SYSTEMS, INC.$600,000NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541710AR72Nov 22, 2004Nov 22, 2004Jun 21, 2007
NNL04AB24P
SBIR PHASE I - HEATED THERMOPLASTIC FIBER PLACEMENT HEAD FOR NASA LANGLEY RESEARCH CENTERACCUDYNE SYSTEMS, INC.$69,714NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——541710AZ11Jan 8, 2004Jan 16, 2004Jul 19, 2004
MSFC0200101DNAS800193
—ACCUDYNE SYSTEMS, INC.$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION——339999All Other Miscellaneous ManufacturingAR91Jan 15, 2001Jan 15, 2001May 15, 2003
LARC0199912DNAS100019
—ACCUDYNE SYSTEMS, INC.$0NATIONAL AERONAUTICS AND SPACE ADMINISTRATION———AR11SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCHDec 15, 1999Dec 15, 1999Jun 15, 2000
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