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ADVANCED TECHNOLOGIES, INC.
Doing business as ADVANCED TECHNOLOGIES INC
NEWPORT NEWS, VA, 23606
Unclaimed
Prime contracting experience
12 records from government sources. Past participation is not evidence of current teaming interest.
| Role | Agency | Description | Vehicle | Obligated | Action date | Period |
|---|---|---|---|---|---|---|
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | DESIGN OF A MODEL-SCALE COAXIAL ROTOR AEROELASTIC TESTBED (MSCRAT) WITH THE INCLUSION OF THREE OPTION PERIODS TO ALLOW FOR FABRICATION OF THE TESTBED, HOVER STAND MODIFICATIONS, AND A MODULAR TAIL CONE, IF EXERCISED. | 80LARC23DA005USAspending | $590,871 | Sep 18, 2026 | Sep 20, 2024 – Oct 31, 2025 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | THIS IS WORK IS FOR THE DETAILED DESIGN AND FABRICATION OF AN ADVANCED ROTORCRAFT TESTBED SUITABLE FOR TESTING A VARIETY OF WINGED COMPOUND ROTORCRAFT CONFIGURATIONS IN THE 14- BY 22-FOOT SUBSONIC TUNNEL BY WAY OF A TRAVERSING ASSEMBLY MOUNTED BELOW A NEW FALSE FLOOR MOUNTED ON ONE OF THE FACILITY'S MODEL CARTS. IN THIS PROJECT, A WINGED COMPOUND HELICOPTER IS DEFINED AS AN AIRCRAFT WITH A CONVENTIONAL ROTOR, LIFTING WINGS, AND CONVENTIONAL TAIL SURFACES. THE ULTIMATE PURPOSE OF THIS TEST EFFORT IS TO GAIN AN UNDERSTANDING OF THE DIFFERENT CONFIGURATION EFFECTS ON THE PERFORMANCE OF COMPOUND ROTORCRAFT TO DRIVE FUTURE ARMY DESIGNS, AND AS SUCH, THE DESIGN SHALL INCORPORATE THE ABILITY TO MEASURE THE INTERACTIONAL EFFECTS OF THE ROTOR WAKE ON THE WING LOCATED AT VARIOUS LOCATIONS, AS WELL AS DIFFERENT TAIL CONFIGURATIONS AND TAIL PROPULSOR CONFIGURATIONS. TESTING WILL INCLUDE THE MEASUREMENT OF ROTOR AND WING LOADS AND MOMENTS AS WELL AS STATIC AND DYNAMIC PRESSURE DATA AT A NUMBER OF LOCATIONS AROUND THE MODEL. THIS TEST CAMPAIGN WILL COVER TWO ENTRIES IN THE 14X22, TENTATIVELY SCHEDULED FOR SUMMER 2019 AND LATE SUMMER/EARLY FALL 2020, AND WILL BE CLOSELY COUPLED WITH A COMPUTATIONAL VALIDATION EFFORT. WHILE THIS SOW IS SPECIFICALLY FOR THE HARDWARE FOR THE FIRST ENTRY, IT IS ANTICIPATED THAT THE MAJORITY OF THE HARDWARE WILL BE UTILIZED FOR THE SECOND ENTRY AS WELL. APPROXIMATELY 95% OF THE DESIGN WORK AND 20% OF THE FABRICATION WAS COMPLETED UNDER RECOM IV. THIS SOW OUTLINES THE TASKS REQUIRED TO COMPLETE THE DESIGN AND FABRICATION UNDER RECOM V. | 80LARC18D0005USAspending | $2,315,162 | Jun 9, 2026 | May 31, 2019 – Sep 30, 2020 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | DESIGN OF A MODEL-SCALE COAXIAL ROTOR AEROELASTIC TESTBED (MSCRAT) WITH THE INCLUSION OF THREE OPTION PERIODS TO ALLOW FOR FABRICATION OF THE TESTBED, HOVER STAND MODIFICATIONS, AND A MODULAR TAIL CONE, IF EXERCISED. | 80LARC23DA005USAspending | $611,925 | Feb 10, 2026 | Dec 10, 2024 – Mar 31, 2026 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | DESIGN, ANALYSIS,&FABRICATION OF C4 BLADE SET 2 DESIGN, ANALYSIS, FABRICATION AND CALIBRATION OF A HIGHLY INSTRUMENTED C4 ROTOR BLADE SET FOR HIGH SPEED FORWARD FLIGHT IN THE 14X22 FOOT SUBSONIC WIND TUNNEL. | 80LARC18D0005USAspending | $505,753 | Sep 11, 2025 | Sep 20, 2019 – Jul 30, 2021 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | FABRICATION OF THE 2.7% SCALE FULL SPAN AND SEMI-SPAN HIGH LIFT COMMON RESEARCH MODEL FOR TESTING IN THE NASA LANGLEY NATIONAL TRANSONIC FACILITY. IT WILL HAVE MODULAR COMPONENTS TO ENABLE THE MODEL TO BE TESTED IN TAKEOFF AND LANDING CONFIGURATIONS. | 80LARC18D0005USAspending | $2,172,930 | Apr 8, 2025 | Jul 27, 2023 – Apr 15, 2025 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | DESIGN AND FABRICATION WORK FOR SWASHPLATELESS PROTOTYPE ROTOR HUB FOR MODEL-SCALE ROTOR TESTING. | 80LARC23DA005USAspending | $381,560 | Dec 9, 2024 | Jul 2, 2024 – Jan 31, 2025 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | DESIGN, ANALYSIS, AND FABRICATION OF COMPOUND TEST HARDWARE. COVERS MULTIPLE ASPECTS WHICH INCLUDE REPAIRING THE LANGLEY ROTOR TEST STAND, UPGRADING COMPONENTS AND INTEGRATING EXISTING HARDWARE TO THE LANGLEY ROTOR TEST STAND. | 80LARC18D0005USAspending | $588,010 | Apr 16, 2024 | Aug 15, 2023 – May 10, 2024 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | WINGED COMPOUND ROTORCRAFT WIND TUNNEL TESTBED. DETAILED DESIGN AND FABRICATION OF AN ADVANCED ROTORCRAFT TESTBED SUITABLE FOR TESTING A VARIETY OF WINGED COMPOUND ROTORCRAFT CONFIGURATIONS IN THE 14 BY 22 FOOT SUBSONIC TUNNEL BY WAY OF A TRAVERSING ASSEMBLY MOUNTED BELOW A NEW FALSE FLOOR MOUNTED ON ONE OF THE FACILITYS MODEL CARTS. IN THIS PROJECT A WINGED COMPOUND HELICOPTER IS DEFINED AS AN AIRCRAFT WITH A CONVENTIONAL ROTOR LIFTING WINGS AND CONVENTIONAL TAIL SURFACES. THE ULTIMATE PURPOSE OF THIS TEST EFFORT IS TO GAIN AN UNDERSTANDING OF THE DIFFERENT CONFIGURATION EFFECTS ON THE PERFORMANCE OF COMPOUND ROTORCRAFT TO DRIVE FUTURE ARMY DESIGNS AND AS SUCH THE DESIGN SHALL INCORPORATE THE ABILITY TO MEASURE THE INTERACTIONAL EFFECTS OF THE ROTOR WAKE ON THE WING LOCATED AT VARIOUS LOCATIONS AS WELL AS DIFFERENT TAIL CONFIGURATIONS AND TAIL PROPULSOR CONFIGURATIONS. | NNL13AA01BUSAspending | $1,437,047 | Mar 5, 2024 | Aug 7, 2018 – Apr 30, 2019 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | FABRICATION OF THE 5.2% SCALE SEMISPAN HIGH LIFT COMMON RESEARCH MODEL (CRM-HL) THE 5.2% SEMISPAN CRM-HL WILL HAVE MODULAR COMPONENTS THAT WILL ENABLE THE MODEL TO BE TESTED IN TAKEOFF, LANDING AND CRUISE CONFIGURATIONS. | 80LARC18D0005USAspending | $1,460,465 | Feb 7, 2023 | Sep 29, 2021 – Feb 28, 2023 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | IGF::OT::IGF DESIGN AND ANALYSIS OF THE ORNITHOPTER WING AN ORNITHOPTER FLAPPING WING WILL BE USED TO INVESTIGATE FLAPPING WING LIFT, THRUST AND POWER CONSUMPTION IN THE EITHER THE NASA LANGLEY 14X22FT WIND-TUNNEL, LOCATED AT NASA LANGLEY RESEARCH CENTER, HAMPTON, VA OR THE ARMY 7X10FT WIND-TUNNEL, LOCATED AT NASA AMES RESEARCH CENTER, MOFFETT FIELD, CA. THE DEVELOPMENT OF A WIND TUNNEL MODEL OF AN ORNITHOPTER FLAPPING WING WILL BE DIVIDED INTO TWO (2) PHASES. THE FIRST PHASE, PHASE I, WILL CONSIST OF THE DESIGN AND ANALYSIS OF A WIND TUNNEL MODEL OF AN ORNITHOPTER FLAPPING WING. THE SECOND PHASE, PHASE II, WILL CONSIST OF THE FABRICATION AND CALIBRATION OF A WIND TUNNEL MODEL OF AN ORNITHOPTER FLAPPING WING. | NNL13AA01BUSAspending | $422,263 | Nov 28, 2022 | Aug 15, 2016 – Oct 31, 2018 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | DESIGN, ANALYSIS, FABRICATION, AND TESTING OF A MACH SCALED ROTOR STAND, THE LANGLEY ROTOR TEST STAND (LRTS). | 80LARC18D0005USAspending | $2,309,840 | Oct 17, 2022 | Sep 24, 2021 – Oct 31, 2022 |
| Prime | National Aeronautics and Space Administration National Aeronautics and Space Administration | DESIGN, ANALYSIS, FABRICATION, AND CALIBRATION OF A MACH SCALED ROTOR BLADE SET AND MODEL SCALE FULLY ARTICULATED ROTOR HUB FOR HIGH SPEED FORWARD FLIGHT IN THE NASA 14X22 FOOT SUBSONIC WIND TUNNEL. | 80LARC18D0005USAspending | $1,507,385 | Sep 29, 2022 | Feb 15, 2022 – Oct 31, 2022 |
Contract vehicles are shown only when present in the source record. Linked award numbers and vehicles open the authoritative record on USAspending.gov.
Subcontracting experience
14 records from government sources. Past participation is not evidence of current teaming interest.
| Role | Agency | Description | Vehicle | Obligated | Action date | Period |
|---|---|---|---|---|---|---|
| Subcontractor | Department of Defense | METAL FABRICATION - COMPLEX - PROVIDE ALL MATERIAL & LABOR TO FABRICATE (QTY. 1) TUBE END PER DRAWING 17-1027, REV. C. VENDOR TO FABRICATE TUBE END FROM STAINLESS STEEL, 17-4H X H1075 CONDITION, PER ASTM A-564. 1036279 Parent award context Parent award agency: Department of Defense · Department of the Air Force Parent award NAICS: 541330 Parent award performance state: TN Parent award description: TEST OPERATIONS AND SUSTAINMENT (TOS) II View parent award on USAspending | — | $99,030 | May 29, 2026 | — – — |
| Subcontractor | Department of Defense | MDR HUB, 3-BLADED PROPROTOR HUB, ELECTRONIC PITCH CONTROL
MFG:AIRMASTER, P/N:AP735 1035928 Parent award context Parent award agency: Department of Defense · Department of the Air Force Parent award NAICS: 541330 Parent award performance state: TN Parent award description: TEST OPERATIONS AND SUSTAINMENT (TOS) II View parent award on USAspending | — | $43,495 | May 20, 2026 | — – — |
| Subcontractor | Department of Defense | 688D,HINGE,STL,DF2157-273#9,REV.C 4500820804 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 336611 Parent award performance state: VA Parent award description: CVN 80 ENGINEERING EFFORTS AND STEEL View parent award on USAspending | — | $47,976 | May 14, 2026 | — – — |
| Subcontractor | Department of Defense | 688D,ASSY,DF3307-197#AY80,REV#K
689D,PLATE,STL,DF420001#14,REV.G
688D,ASSY,DF3307-197#AY80,REV#K
688D,NIPPLE,CUNI,DF2203-130#4,REV.C
689D,CHANNEL,STL,DF2155-659#932,REV.K
688D, PIN STL, DF2157-276 #86, REV. F 4500813215 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 336611 Parent award performance state: VA Parent award description: CVN 80 ENGINEERING EFFORTS AND STEEL View parent award on USAspending | — | $88,990 | Feb 25, 2026 | — – — |
| Subcontractor | Department of Defense | 689D,HINGE FRAME,DF9081-166#3,REV#R
689D,HINGE FRAME,DF9081-166#3,REV#R 4500812246 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 336611 Parent award performance state: VA Parent award description: CVN 80 ENGINEERING EFFORTS AND STEEL View parent award on USAspending | — | $83,941 | Feb 17, 2026 | — – — |
| Subcontractor | Department of Defense | 688D,DOOR WLDMNT,LH,DF1520-94#2,REV. E 4500807621 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 336611 Parent award performance state: VA Parent award description: CVN 80 ENGINEERING EFFORTS AND STEEL View parent award on USAspending | — | $43,880 | Dec 10, 2025 | — – — |
| Subcontractor | Department of Defense | AEROSPACE SUPPORT 4800043856 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 334511 Parent award performance state: CA Parent award description: IGF::OT::IGF XLUUV(ORCA)SYSTEM DESIGN&TECH DATA PKG View parent award on USAspending | — | $475,540 | Jan 30, 2025 | — – — |
| Subcontractor | Department of Defense | AEROSPACE SUPPORT 4800044395 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 334511 Parent award performance state: CA Parent award description: IGF::OT::IGF XLUUV(ORCA)SYSTEM DESIGN&TECH DATA PKG View parent award on USAspending | — | $31,120 | Jan 24, 2025 | — – — |
| Subcontractor | Department of Defense | AEROSPACE SUPPORT 4800043131 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 334511 Parent award performance state: CA Parent award description: IGF::OT::IGF XLUUV(ORCA)SYSTEM DESIGN&TECH DATA PKG View parent award on USAspending | — | $40,100 | Dec 10, 2024 | — – — |
| Subcontractor | Department of Defense | SUBCONTRACT FUNDING 187251 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 541715 Parent award performance state: MD Parent award description: BERTICAL TAKEOFF AND LANDING FAMILY OF SYSTEMS View parent award on USAspending | N0002422D6404USAspending | $853,490 | Mar 8, 2024 | — – — |
| Subcontractor | Department of Defense | SUBCONTRACT FUNDING 178796 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 541712 Parent award performance state: MD Parent award description: FUTURE VERTICAL LIFT DEVELOPMENT View parent award on USAspending | N0002413D6400USAspending | $63,990 | Aug 3, 2023 | — – — |
| Subcontractor | Department of Defense | DESIGN OF UNIQUE AERODYNAMIC CONFIGURATIONS 178796 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 541712 Parent award performance state: MD Parent award description: FUTURE VERTICAL LIFT DEVELOPMENT View parent award on USAspending | N0002413D6400USAspending | $263,985 | May 24, 2023 | — – — |
| Subcontractor | Department of Defense | SUBCONTRACT FUNDING 178796 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 541712 Parent award performance state: MD Parent award description: FUTURE VERTICAL LIFT DEVELOPMENT View parent award on USAspending | N0002413D6400USAspending | $382,235 | Oct 26, 2022 | — – — |
| Subcontractor | Department of Defense | FATHOMETER FAIRING 4104368962 Parent award context Parent award agency: Department of Defense · Department of the Navy Parent award NAICS: 336611 Parent award performance state: MD Parent award description: MMSC DETAILED DESIGN AND CONSTRUCTION View parent award on USAspending | — | $88,350 | Sep 26, 2022 | — – — |
Contract vehicles are shown only when present in the source record. Linked award numbers and vehicles open the authoritative record on USAspending.gov.
Agencies supported
- National Aeronautics and Space AdministrationGov-sourced