TRANSPORTATION R&D SERVICES; AEROSPACE RESEARCH; APPLIED RESEARCH

WA-10-03770-- INCREMENTAL FUNDING - NEXTGEN HD TRAJECTORY MGMT-ARRIVAL TACTICAL FLOW_TBFM_ PROGRAM 'NEW CONTRACT'. TO PROVIDE PROGRAM MANAGEMENT, SYSTEMS ENGINEERING, SYSTEM DESIGN, SYSTEM TEST AND EVALUATION, TRAINING, IMPLEMENTATION, INTEGRATED LOGISTICS SUPPORT & ENGINEERING SUPPORT. TENTATIVE CONTRACT DTFAWA-10-C-00052. PERIOD OF PERFORMANCE --TBD (BASE PERIOD (5 YEARS) WITH 5 OPTION YEARS A TOTAL OF 10 YEARS) 10-AJR4500-6000 TAS::69 8107::TAS

THE PURPOSE OF THIS ACTION IS TO ISSUE TASK ORDER 2 UNDER THE DFO2 IDIQ FOR TECHNICAL REFRESH AND ENHANCEMENT TASKS.

THE PURPOSE OF THIS ACTION IS TO ISSUE TASK ORDER 1 UNDER THE DFO2 IDIQ FOR PROGRAM MANAGEMENT TASKS.

MICRO-X - PASSENGER SELF SCREENING BAA CALL TTA 1

THE PURPOSE OF THIS ACTION IS TO ISSUE TASK ORDER 3 UNDER THE DFO2 IDIQ FOR CONTRACTOR DEPOT LOGISTICS SUPPORT (CDLS) TASKS.

NO COST EXTENSION

THE PURPOSE OF MODIFICATION P00008 IS TO DEOBLIGATE UNEXPENDED FUNDING AND CLOSEOUT THE CONTRACT

TASK ORDER 4 ENGINEERING SERVICES IN SUPPORT OF THE WIDE AREA AUGMENTATION SYSTEM (WAAS) DUAL FREQUENCY OPERATIONS (DFO) 2 [DFO-2].

FABRICATE AND FACILITATE THE USE OF THE SILICON CARBIDE/SILICON CARBIDE MATERIALS IN AEROSPACE STRUCTURES. THE MATERIAL PROPERTY ALLOWABLES NEED TO BE CHARACTERIZED FOR A VARIETY OF LAYUPS OVER A RANGE OF TEMPERATURES UTILIZING MELT INFILTRATION (MI)

A GROUP OF CHEMICAL VAPOR INFILTRATION (CVI) PROCESSED CARBON SILICON CARBIDE (C/SIC) AND SILICON CARBIDE/SILICON CARBIDE (SIC/SIC) COMPONENTS ARE REQUIRED FOR MANUFACTURING DEMONSTRATIONS AND MATERIAL/COMPONENT PERFORMANCE TESTING.

DEVELOPING A DESIGN OF A DUAL FLOW PATH NOZZLE FOR A TURBINE BASED COMBINED CYCLE PROPULSION SYSTEM.

A GROUP OF CHEMICAL VAPOR INFILTRATION (CVI) PROCESSED CARBON SILICON CARBIDE (C/SIC) AND SILICON CARBIDE/SILICON CARBIDE (SIC/SIC) COMPONENTS ARE REQUIRED FOR MANUFACTURING DEMONSTRATIONS AND MATERIAL/COMPONENT PERFORMANCE TESTING.

A GROUP OF MELT INFILTRATION (MI) PROCESSED SILICON CARBIDE/SILICON CARBIDE (SIC/SIC).AERODYNAMIC CONTROL SURFACES ARE REQUIRED FOR MANUFACTURING DEMONSTRATIONS AND.MATERIAL/COMPONENT PERFORMANCE TESTING.

FABRICATION OF SILICON CARBIDE/SILICON CARBIDE (SIC/SIC) PANELS FOR CHARACTERIZATION UTILIZING THE MELT INFILTRATION (MI) DENSIFICATION PROCESS.

REUSABLE CMC HOT STRUCTURES FOR HYPERSONIC TECHNOLOGY DEVELOPMENT AT NASA LARC.

THE CONTRACTOR SHALL FABRICATE SILICON CARBIDE/SILICON CARBIDE (SIC/SIC) PANELS FOR CHARACTERIZATION UTILIZING THE MELT INFILTRATION (MI) AND CHEMICAL VAPOR INFILTRATION (CVI) DENSIFICATION PROCESSES.

NON-RECURRING ENGINEERING (NRE) SERVICES REQUIRED TO FABRICATE A TOTAL OF THIRTY-TWO ARTICLES USING CVI SIC DENSIFICATION OF SILICON CARBIDE FIBER PREFORMS, IN SUPPORT OF CVI SIC/SIC CMC TECHNOLOGY MATURATION AT NASA GLENN RESEARCH CENTER (GRC).

NEXTOR SMALL AIRCRAFT PH3 - FUNDING ACTION

IDSS REMOTE SCREENING SBIR PHASE III

VALIDATION OF ADVANCED LINER CONCEPTS VIA STATIC ENGINE TEST

CERAMIC MATRIX COMPOSITE HEAT EXCHANGER FOR HYPERSONIC TECHNOLOGY DEVELOPMENT. FABRICATE AND TEST ACTIVELY COOLED CERAMIC MATRIX COMPOSITE COMPONENTS FOR HYPERSONIC AIRBREATHING PROPULSION SYSTEMS.

NEXTOR III - AI & ADVANCES ANALYTICS TO ESTIMATE COLLISION RISK DURING DEPARTURE & ARRIVAL TASK ORDER AWARD

NEXTOR III - DRONE INCURSION FORECASTING SYSTEM SAFETY MANAGEMENT TRANSFORMATION (SSMT)

NEXTOR III - SMALL AIRCRAFT RUNWAY LENGTH ANALYSIS TOOL (SARLAT)

NEXTOR III - FAA MAINTENANCE SCHEDULE OPTIMIZATION