Summary
DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL has no OSHA inspection history on file. Federal records covering wage, environmental, labor relations, and other agencies are noted below where present.
The most recent federal enforcement activity was recorded 0 days ago.
Federal records were found in 1 of 15 sources. Sources without matching records returned empty for this establishment.
Agency coverage
DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL appears in NHTSA vehicle recalls record only. No matching records were found in OSHA workplace safety, WHD wage enforcement, MSHA mine safety, EPA environmental compliance, NLRB labor relations, OFLC visa and labor certification (historical), FMCSA motor carrier registration, SAM.gov federal debarment, CMS nursing home enforcement, UVA Corporate Prosecution Registry, or CPSC product recalls. Single-agency enforcement records typically indicate either a discrete incident-based inspection or a low-risk operational profile.
OSHA workplace safety
No OSHA inspections, citations, or accidents on file for DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL. Verify directly with Occupational Safety and Health Administration →
Safety self-report (OSHA 300A)
No self-reported injury rates filed with OSHA's Injury Tracking Application for DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL. Verify directly with OSHA Injury Tracking Application →
OSHA severe injury reports
No severe injury reports (hospitalization, amputation, or loss of an eye) on file under 29 CFR 1904.39 for DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL. Verify directly with Occupational Safety and Health Administration →
Activity timeline
Most recent federal enforcement activity recorded 0 days ago. Data on this page is refreshed weekly.
Wage & Hour Division (WHD)
No WHD wage, overtime, or child-labor enforcement cases on file for DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL. Verify directly with Wage and Hour Division →
Mine safety (MSHA)
No MSHA mine safety violations on file for DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL. Verify directly with Mine Safety and Health Administration →
Labor relations (NLRB)
No NLRB unfair labor practice charges or union representation cases on file for DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL. Verify directly with National Labor Relations Board →
Visa & labor certification (OFLC) — historical
No H-1B, H-2A, or H-2B labor condition applications on file (historical data only — DOL ended OFLC publication) for DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL. Verify directly with Office of Foreign Labor Certification →
Environmental compliance (EPA)
No EPA inspections or formal enforcement actions on file for DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL. Verify directly with Environmental Protection Agency →
Federal criminal prosecution record
No federal criminal prosecutions, plea agreements, or deferred-prosecution agreements on file for DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL. Verify directly with UVA Corporate Prosecution Registry →
NHTSA vehicle & equipment recalls
Most-recalled component: ELECTRICAL SYSTEM:SOFTWARE. Most recent campaign: 2014-07-15. Source: National Highway Traffic Safety Administration, matched on manufacturer name.
Federal contracts
This location
- Department of DefenseSBIR PHASE II.5 TOPIC N07-006contract · Last action 2013-10-18$1,499,047
- Department of DefenseSBIR PHASE IIcontract · Last action 2012-11-26$1,249,437
- Department of DefenseRESEARCH AND DEVELOPMENT BAA RFP# - ARMY-FY18-44-RDECOM07contract · Last action 2021-08-16$999,910
- Department of DefenseIGF::OT::IGF STTR PHASE IIcontract · Last action 2018-01-23$999,804
- Department of DefenseIGF::OT::IGF RESEARCH AND DEVELOPMENTcontract · Last action 2018-12-21$999,581
- National Aeronautics and Space AdministrationIGF::OT::IGF RESEARCH IS PROPOSED TO DEMONSTRATE THE USE OF ADVANCED MANUFACTURING TECHNIQUES TO ENABLE THE AFFORDABLE APPLICATION OF MULTI-FUNCTIONAL THERMAL/ENVIRONMENTAL BARRIER COATINGS (T/EBCS) HAVING ENHANCED RESISTANCE TO HIGH TEMPERATURE COMBUSTION ENVIRONMENTS. T/EBCS ARE ENVISIONED TO PROTECT THE SURFACE OF SI-BASED CERAMICS AGAINST MOISTURE-ASSISTED, OXIDATION-INDUCED CERAMIC RECESSION. CURRENT T/EBC SYSTEMS HAVE BEEN DEMONSTRATED IN LONG TIME EXPOSURES AT ~2400 F SUBSTRATE TEMPERATURES. HOWEVER, THEIR USE AT ELEVATED TEMPERATURES (I.E., 2700 F SUBSTRATE TEMPERATURES) IS LIMITED BY THE LOW TEMPERATURE STABILITY AND HIGH DIFFUSION ACTIVITY OF CURRENT T/EBC MATERIALS. ONE APPROACH TO INCREASE THE TEMPERATURE CAPABILITY OF THESE SYSTEMS IS THE INCORPORATION OF MULTILAYERED T/EBC DESIGNS. IN THIS EFFORT, ENHANCED PROCESSING TECHNIQUES WILL BE EMPLOYED TO DEMONSTRATE THE MANUFACTURE OF ROBUST T/EBC SYSTEMS USING A PHYSICAL VAPOR DEPOSITION BASED PROCESSING APPROACH WHICH ENABLES IMPROVED COATING ADHESION AND ADVANCED COATING ARCHITECTURAL, COMPOSITIONAL, AND MICROSTRUCTURAL CONTROL, AS WELL AS NON-LINE-OF-SIGHT (NLOS) DEPOSITION. DURING THIS PROPOSED PHASE II EFFORT, PROCESSING/PROPERTY/PERFORMANCE RELATIONSHIPS FOR THE MANUFACTURE OF THE NOVEL COATING ARCHITECTURES WILL BE DETERMINED. OPTIMIZED PROCESSING APPROACHES WILL THEN BE USED TO DEMONSTRATE THE DEPOSITION OF HIGH TEMPERATURE CAPABLE T/EBC SYSTEMS COATING ONTO COMPONENTS OF INTEREST TO GAS TURBINE ENGINE MANUFACTURERS.contract · Last action 2018-07-20$901,160
- National Aeronautics and Space AdministrationIGF::OT::IGF NASA'S LONG RANGE GOALS OF REDUCING FUEL CONSUMPTION BY 30% AND INCREASING FUEL EFFICIENCY BY 35% CAN BE PARTIALLY ACCOMPLISHED THROUGH INCREASING THE OPERATION TEMPERATURES OF GAS TURBINE ENGINES. THE ADVENT OF ADVANCED ALLOYS, COATINGS, COOLING TECHNOLOGIES AND CERAMIC COMPONENTS HAS CREATED THE POTENTIAL FOR SIGNIFICANT INCREASES IN THE HOT SECTION OF THESE ENGINES; HOWEVER, THESE ADVANCES WILL ALSO LEAD TO ELEVATED TEMPERATURES IN OTHER REGIONS OF THE ENGINE. FOR EXAMPLE, THE TURBINE DISK SECTION WOULD ALSO NEED TO OPERATE AT INCREASINGLY HIGHER TEMPERATURES THAT WOULD SUBJECT IT TO OXIDATION AND HOT CORROSION DEGRADATION MECHANISMS NOT CURRENTLY EXPERIENCED. ONE APPROACH TO ENHANCE THE TEMPERATURE CAPABILITY OF THESE SYSTEMS IS THROUGH THE INCORPORATION OF ENVIRONMENTAL PROTECTIVE COATINGS. RESEARCH IS PROPOSED HERE TO EMPLOY ADVANCED COATING MANUFACTURING TECHNIQUES DESIGNED TO ENABLE THE AFFORDABLE APPLICATION OF ENVIRONMENTAL PROTECTIVE COATINGS HAVING ENHANCED RESISTANCE TO HOT CORROSION AND OXIDATION. ADVANCED TESTING APPROACHES WILL BE USED THAT SIMULATE REAL-WORLD CONDITIONS AND DEMONSTRATE THE PERFORMANCE ADVANTAGES OF THE DEPOSITED COATINGS. THE COATING SYSTEMS WILL BE APPLIED IN THIS WORK ONTO COUPONS AND COMPONENTS TO DEMONSTRATE COATING CAPABILITY AND ALLOW SIMULATED ENGINE ENVIRONMENT TESTING IN FOLLOW-ON PROGRAMS.contract · Last action 2016-07-20$868,601
- Department of DefenseRESEARCH AND DEVELOPMENT, STTR PHASE II, IGF::OT::IGFcontract · Last action 2021-03-15$816,732
- Department of Defense(STTR PHASE II) HIGH-TEMPERATURE ENVIRONMENTAL BARRIER COATING FOR SILICON CARBIDE COMPOSITEScontract · Last action 2011-03-23$749,957
- Department of Defense200606!352518!1700!N68335!NAVAL AIR ENGINEERING STATION !N6833506C0068 !A!N! !Y! ! !20060323!20060323!036500804!036500804!036500804!N!DIRECTED VAPOR TECHNOLOGIES IN!2 BOARS HEAD LANE !CHARLOTTESVILL !VA!22903!14968!540!51!CHARLOTTESVILLE !CHARLOTTESVILLE (CITY)!VIRGINIA !+000000499659!N!N!000001999078!AC62!RDTE/ELECTRONICS & COMMUNICATION EQ-APPLIED RESEA !C9E!ALL OTHER SUPPLIES AND EQUIPMENT !000 !NOT DISCERNABLE !541710!E! !3! ! ! ! ! !99990909!B! ! !B! !A!U!U!2!023!K! !Z!Y!Z! ! !N!B!N!N! ! !Z! !B!A!000!C!B!N! ! ! ! !1719!N00421!0001! !contract · Last action 2011-03-16$749,683
- Department of DefenseSBIR PHASE II TOPIC N101-036contract · Last action 2013-03-21$749,517
- Department of DefenseR&D SBIR PHASE II TOPIC N07-006contract · Last action 2009-08-05$749,507
- Department of DefenseIGF::OT::IGF OPTIMIZING COATING PROCESSES AND CHEMISTRIES FOR ENHANCED HOT SECTION, LOW CYCLE FATIGUE (LCF) LIFEcontract · Last action 2014-08-11$749,251
- Department of DefenseRESEARCH AND DEVELOPMENT SBIR TOPIC N093-180contract · Last action 2011-07-19$749,028
- Department of DefenseSBIR PHASE IIcontract · Last action 2013-06-13$748,936
- Department of DefenseIGF::OT::IGF SBIR II- HYDRATIONTOLERANT, LOW THERMAL CONDUCTIVITYcontract · Last action 2015-11-13$737,480
- Department of DefenseDIRECTED VAPOR SBIR II MULITFUNCTIONAL DAMPING COATINGcontract · Last action 2013-08-22$736,940
- Department of DefenseSBIR PHASE II, TOPIC #:A06-082contract · Last action 2010-01-05$729,701
- Department of DefenseR & D SBIR PHASE II TOPIC N06-032contract · Last action 2008-01-23$349,824
- Department of DefenseRESEARCH AND DEVELOPMENT IGF::OT::IGFcontract · Last action 2018-07-24$224,744
- Department of DefenseSBIR I HYDRATION TOLERANT LOW THERMAL CONDUCTIVITY (K) THERMAL BARRIER COATINGScontract · Last action 2012-05-15$149,932
- Department of DefenseIGF::OT::IGF PHASE I FIRST MONTHLY TECHNICAL REPORTcontract · Last action 2017-08-09$149,772
- Department of DefenseSBIR PHASE I CONTRACTcontract · Last action 2010-09-22$149,745
- Department of DefenseIGF::OT::IGF PHASE I FIRST MONTHLY TECHNICAL REPORTcontract · Last action 2014-08-25$149,720
- Department of DefenseR&D SBIR TOPIC N101-036contract · Last action 2011-05-10$149,694
- Department of DefenseSBIR Icontract · Last action 2012-05-25$149,690
- Department of DefenseIGF::CT::IGF SBIRSOL2015.1contract · Last action 2016-05-05$149,528
- National Aeronautics and Space AdministrationRESEARCH IS PROPOSED TO INVESTIGATE THE FEASIBILITY OF USING ADVANCED MANUFACTURING TECHNIQUES TO ENABLE THE AFFORDABLE APPLICATION OF MULTI-FUNCTIONAL HIGH TEMPERATURE COATINGS HAVING ENHANCED RESISTANCE TO HIGH TEMPERATURE ENGINE ENVIRONMENTS. FOR EXAMPLE, THERMAL / ENVIRONMENTAL BARRIER COATINGS (T/EBCS) ARE ENVISIONED TO PROTECT THE SURFACE OF SI-BASED CERAMICS AGAINST MOISTURE-ASSISTED, OXIDATION-INDUCED CERAMIC RECESSION. CURRENT T/EBC SYSTEMS HAVE BEEN DEMONSTRATED IN LONG TIME EXPOSURES AT ~2400?F. HOWEVER, THEIR USE AT ELEVATED TEMPERATURES IS LIMITED BY THE LOW TEMPERATURE STABILITY AND HIGH DIFFUSION ACTIVITY OF CURRENT T/EBC MATERIALS. ONE APPROACH TO ENHANCE THE TEMPERATURE CAPABILITY OF THESE SYSTEMS IS THE INCORPORATION OF MULTI-LAYERED T/EBC DESIGNS TO PROVIDE MULTI-FUNCTIONAL PROTECTION. IN THIS PHASE I EFFORT, NOVEL PROCESSING TECHNIQUES WILL BE DEVELOPED TO ENABLE THE AFFORDABLE, HIGH PERFORMANCE MANUFACTURE OF SUCH SYSTEMS USING A PHYSICAL VAPOR DEPOSITION BASED PROCESSING APPROACH WHICH ENABLES ENHANCED COATING ADHESION AND ADVANCED COATING ARCHITECTURAL, COMPOSITIONAL AND MICROSTRUCTURAL CONTROL. PROCESSING DEVELOPMENTS WILL THEN BE USED TO CREATED NOVEL MULTI-LAYERED COATINGS. THESE COATING LAYERS WILL THEN BE INCORPORATED INTO ADVANCED HIGH TEMPERATURE CAPABLE T/EBC SYSTEMS IN PHASE. THIS WORK WILL LEAD TO THE INCORPORATION OF SI-BASED CERAMIC COMPONENTS INTO ENHANCED EFFICIENCY GAS TURBINE ENGINES TO REDUCE WEIGHT AND INCREASE OPERATING TEMPERATURES. A TRL 4 WILL BE ACHIEVED AT THE END OF PHASE I AND TRL 6 AT THE END OF PHASE II.contract · Last action 2012-02-13$124,694
- National Aeronautics and Space AdministrationIGF::OT::IGF NASA'S LONG RANGE GOALS OF REDUCING THE FUEL CONSUMPTION BY 30% AND INCREASING FUEL EFFICIENCY BY 35% CAN BE PARTIALLY ACCOMPLISHED THROUGH INCREASING ENGINE OPERATION TEMPERATURES. AS A RESULT, THE DISK SECTION IS DESIRED TO OPERATE IN INCREASINGLY HIGHER TEMPERATURES, WHICH WILL SUBJECT IT TO ADDITIONAL DEGRADATION MECHANISMS OF OXIDATION AND HOT CORROSION. ONE APPROACH TO ENHANCE THE TEMPERATURE CAPABILITY OF THESE SYSTEMS IS THROUGH THE INCORPORATION OF ENVIRONMENTAL PROTECTIVE COATINGS WHICH CAN PROVIDE RESISTANCE FROM OXIDATION AND HOT CORROSION. RESEARCH IS PROPOSED HERE TO OPTIMIZE THE USE OF ADVANCED COATING MANUFACTURING TECHNIQUES DESIGNED TO ENABLE THE AFFORDABLE APPLICATION OF ENVIRONMENTAL PROTECTIVE COATINGS HAVING ENHANCED RESISTANCE TO HOT CORROSION AND OXIDATION TO ALLOW OPERATION AT THE DESIRED HIGH TEMPERATURE ENGINE ENVIRONMENTS. ADVANCED TESTING CONDITIONS WILL BE USED TO SIMULATE REAL WORLD CONDITIONS AND DEMONSTRATE THE PERFORMANCE OF THE DEPOSITED COATINGS IN THESE CONDITIONS. THIS APPROACH IS ENVISIONED TO AID THE DEVELOPMENT OF ADVANCED COATINGS REQUIRED TO PROTECT THE SURFACE OF TURBINE DISK COMPONENTS AT HIGHER TEMPERATURES DESIRED FOR FUEL AND THRUST OPERATIONALLY IMPROVEMENT WITHOUT INDUCING SIGNIFICANT FATIGUE DEBIT. ADVANCED COATING SYSTEMS WILL BE APPLIED IN THIS WORK ONTO COUPONS, AND SUBCOMPONENTS TO DEMONSTRATE COATING CAPABILITY AND ALLOW SIMULATED ENGINE ENVIRONMENT TESTING IN FOLLOW ON PROGRAMS. SUCCESS IN MEETING THE OBJECTIVES WILL SIGNIFICANTLY AID THE TEMPERATURE CAPABILITY OF TURBINE DISK COMPONENTS, ALLOWING SIGNIFICANT FUEL EFFICIENCY AND THRUST INCREASES FOR TURBINE ENGINES.contract · Last action 2014-02-14$123,970
- National Aeronautics and Space AdministrationIGF::OT::IGF RESEARCH IS PROPOSED TO DEMONSTRATE THE USE OF ADVANCED MANUFACTURING TECHNIQUES TO ENABLE THE AFFORDABLE APPLICATION OF MULTI-FUNCTIONAL THERMAL / ENVIRONMENTAL BARRIER COATINGS (T/EBCS) HAVING ENHANCED RESISTANCE TO HIGH TEMPERATURE COMBUSTION ENVIRONMENTS. T/EBCS ARE ENVISIONED TO PROTECT THE SURFACE OF SI-BASED CERAMICS AGAINST MOISTURE-ASSISTED, OXIDATION-INDUCED CERAMIC RECESSION. CURRENT T/EBC SYSTEMS HAVE BEEN DEMONSTRATED IN LONG TIME EXPOSURES AT ~2400 F SUBSTRATE TEMPERATURES. HOWEVER, THEIR USE AT ELEVATED TEMPERATURES (I.E. 2700 F SUBSTRATE TEMPERATURES) IS LIMITED BY THE LOW TEMPERATURE STABILITY AND HIGH DIFFUSION ACTIVITY OF CURRENT T/EBC MATERIALS. ONE APPROACH TO INCREASE THE TEMPERATURE CAPABILITY OF THESE SYSTEMS IS THE INCORPORATION OF MULTI-LAYERED T/EBC DESIGNS. IN THIS PHASE I EFFORT, ENHANCED PROCESSING TECHNIQUES WILL BE EMPLOYED TO DEMONSTRATE THE MANUFACTURE OF ROBUST T/EBC BOND COAT SYSTEMS USING A PHYSICAL VAPOR DEPOSITION BASED PROCESSING APPROACH WHICH ENABLES IMPROVED COATING ADHESION AND ADVANCED COATING ARCHITECTURAL, COMPOSITIONAL AND MICROSTRUCTURAL CONTROL, AS WELL AS NON-LINE-OF-SIGHT (NLOS) DEPOSITION. SCALED PROCESSING APPROACHES WILL THEN BE USED TO DEMONSTRATE THE DEPOSITION OF HIGH TEMPERATURE CAPABLE T/EBC BOND COATS ONTO COMPONENTS OF INTEREST TO GAS TURBINE ENGINE MANUFACTURERS. THESE BOND COATS WILL THEN BE INCORPORATED INTO FULL HIGH TEMPERATURE CAPABLE T/EBC SYSTEMS PLANNED IN PHASE II. FINALLY, CONCEPTS TO ENABLE THE DEPOSITION OF T/EBC BOND COAT SYSTEMS ON NLOS INTERNAL REGIONS OF HOLLOW COMPONENTS WILL BE INVESTIGATED. THIS WORK WILL SIGNIFICANTLY AID THE INCORPORATION OF SI-BASED CERAMIC COMPONENTS IN GAS TURBINE ENGINES RESULTING IN REDUCED WEIGHT AND INCREASED OPERATING TEMPERATURES.contract · Last action 2014-05-19$121,972
- National Aeronautics and Space AdministrationIGF::OT::IGF DVTI TO USE THEIR DVD COATING PROCESS IN APPLYING TWO COATING COMPOSITIONS SPANNING NASA RANGE OF INTEREST. - COATINGS: TWO, PERHAPS FIGURE NI30CR0.1Y AND NI45CR0.1Y, EACH COATING COMPOSITION MEASURED AFTER APPLICATION ON THE SPECIMEN - LSHR FATIGUE SPECIMENS (DESIGN AS BEFORE) TO COAT FOR EACH COATING: 16 (TEST 800F) + 16 (TEST 1400F) + 16 (EXPOSE PLUS TEST 1400F) PLUS 2 SPARES = 50 SPECIMENS PER COATING, 100 SPECIMENS TOTAL - LSHR PINS (0.25 DIAMETER) TO COAT FOR EACH COATING: 8 SPECIMENS PER EACH COATING, 16 SPECIMENS TOTAL - LSHR COUPONS (0.5 WIDE, 1.0 LONG, 0.125 THICK TO COAT FOR EACH COATING: 8 SPECIMENS PER EACH COATING, 16 SPECIMENS TOTAL - PRE-TREATMENTS BEFORE COATING: ONE PRE-TREATMENT TO BE DECIDED AND APPLIED BY DVTI, POSSIBLY SHOT PEENING PLUS PLASMA ETCHEDcontract · Last action 2017-08-18$119,200
- Department of DefenseSTTR (PHASE 1) - HIGH TEMPERATURE ENVIRONMENTAL BARRIER COATING FOR SILICON CARBIDE COMPOSITEScontract · Last action 2009-06-04$99,971
- Department of DefenseDEVELOPMENT OF MULTIFUNCTIONAL DAMPING COATING SYSTEMS FOR TURBINE ENGINE COMPONENTScontract · Last action 2010-03-17$99,968
- Department of DefenseDIRECTED VAPOR TECHcontract · Last action 2008-01-07$99,900
- Department of DefenseAF SBIR I; FA093-168; ELECTRON BEAMcontract · Last action 2010-03-12$99,864
- Department of DefenseIGF::OT::IGF SBIR PH I SELF REGENERATIVE COATINGS FOR ENHANCED PROTECTION OF SILICON BASED CERAMIC COMPOSITES IN PARTICLE LADEN DEGRADED ENGINE ENVIRONMENTScontract · Last action 2017-08-09$99,785
- Department of DefenseSBIR Icontract · Last action 2008-05-19$99,765
- National Aeronautics and Space AdministrationADVANCED ENVIRONMENTAL BARRIER COATING PROCESSING AND DEVELOPMENT FOR SIC/SIC CMC COMPONENTScontract · Last action 2013-07-09$94,000
- Department of DefenseIGF::CT::IGF SBIRSOL2016.1contract · Last action 2016-10-18$79,925
- Department of DefenseRESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)contract · Last action 2012-06-18$79,812
- Department of DefenseR&D SBIR PHASE I TOPIC N07-006contract · Last action 2008-01-15$69,909
- National Aeronautics and Space AdministrationAPPLY COATINGS ON PROVIDED SUBSTRATEScontract · Last action 2010-06-04$65,000
- National Aeronautics and Space AdministrationCOATING SERVICEcontract · Last action 2012-05-09$64,000
- National Aeronautics and Space AdministrationPROCESS BARRIER COATING SYSTEMcontract · Last action 2010-12-29$64,000
- National Aeronautics and Space AdministrationIGF::OT::IGF BOND COAT APPLICATION RUNS AND TOP COAT APPLICATION RUNScontract · Last action 2016-04-13$62,450
- National Aeronautics and Space AdministrationADVANCED ENVIRONMENTAL BARRIER COATING PROCESSING AND DEVELOPMENT FOR SIC/SIC CMC COMPONENTScontract · Last action 2013-11-05$60,000
- National Aeronautics and Space AdministrationIGF::OT::IGF DIRECTED VAPOR ELECTRON BEAM - PHYSICAL VAPOR DEPOSITION NASA COMPOSITION ENVIRONMENTAL BARRIER COATING SYSTEMScontract · Last action 2017-02-08$57,300
- National Aeronautics and Space AdministrationENVIRONMENTAL BARRIER COATING PROCESS DESPOSITIONcontract · Last action 2017-02-10$49,970
- National Aeronautics and Space AdministrationIGF::OT::IGF NONMETALLIC FABRICATED MATERIALScontract · Last action 2018-09-10$46,050
- National Aeronautics and Space AdministrationADVANCED ENVIRONMENTAL BARRIER COATING PROCESSING AND DEVELOPMENT FOR SIC/SIC CMC COMPONENTScontract · Last action 2013-04-25$38,000
Federal contract dollars to this establishment. Primary NAICS: 541712 - RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY). Last action: 2021-08-16. Source: USAspending.gov, net obligations. Recipient address is the SAM registration / HQ address, not necessarily the worksite.
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About this data
This profile aggregates federal enforcement records on DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL from every major federal compliance and enforcement source plus the UVA Corporate Prosecution Registry. OSHA workplace safety inspections, WHD wage cases, MSHA mine safety, EPA environmental enforcement, NLRB labor relations, OFLC visa/labor certification, FMCSA motor carrier registration, SAM.gov debarments, CMS nursing-home records, BLS industry safety benchmarks, OSHA ITA self-reported injury rates, SEC enforcement and financial disclosures, CPSC and NHTSA recalls.
Establishments are matched across agencies using normalized employer name, state, and ZIP code.
OSHA citations typically appear 3–8 months after the inspection, so very recent enforcement actions may not yet be reflected. Profiles may be incomplete if the establishment operates under multiple legal names or files under variations our entity-matching rules don’t yet cover. To report a missing record or correction, email corrections@fastdol.com.
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Contact sales →Frequently asked
- What is DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL's OSHA violation history?
- DIRECTED VAPOR TECHNOLOGIES INTERNATIONAL has no OSHA inspections on record.