THE BOEING COMPANY

IGF::OT::IGF ARC JET TEST IN SUPPORT OF FLEXIBLE THERMAL PROTECTION SYSTEM EVALUATION AND DEVELOPMENT THE SCOPE OF THIS TASK ORDER IS TO EVALUATE FTPS LAYUPS AND MATERIALS AT COMPARABLE OR HARSHER SIMULATED ATMOSPHERIC REENTRY FLIGHT CONDITIONS. FTPS MATERIALS AND SYSTEMS WILL BE TESTED UTILIZING THE TEST FACILITY FOR UP TO 10 WEEKS OF TOTAL TEST TIME AT THREE SPECIFIC TEST CONDITIONS THAT SIMULATE RELEVANT TEST ENVIRONMENTS.THE OBJECTIVES FOR THIS TASK ORDER ARE AS FOLLOWS: OBJECTIVE ONE: EVALUATION OF FTPS LAYUPS AND MATERIALS AT FLIGHT-LIKE CONDITIONS SIMULATING A HEAT FLUX ENTRY CONDITION (SQUARE PULSE OR MISSION PROFILE IN STAGNATION OR SHEAR) OF 50 W/CM2 (HEAT FLUX BETWEEN 17 AND 50 W/CM2, PRESSURE BETWEEN 1.7 AND 10KPA). OBJECTIVE TWO: EVALUATION OF FTPS LAYUPS AND MATERIALS AT FLIGHT-LIKE CONDITIONS SIMULATING A HEAT FLUX ENTRY CONDITION (SQUARE PULSE OR MISSION PROFILE IN STAGNATION OR SHEAR) OF 50-75 W/CM2 (HEAT FLUX BETWEEN 50 AND 75 W/CM2, PRESSURE BETWEEN 3 AND 6KPA). OBJECTIVE THREE: EVALUATION OF FTPS LAYUPS AND MATERIALS AT FLIGHT-LIKE CONDITIONS SIMULATING A HEAT FLUX ENTRY CONDITION (SQUARE PULSE OR MISSION PROFILE IN STAGNATION OR SHEAR) OF 75-130 W/CM2 (HEAT FLUX BETWEEN 75 AND 130 W/CM2, PRESSURE BETWEEN 3 AND 10 KPA).

THE BOEING COMPANY CONTRACT 693KA7-21-C-00010 TO FUND FUTURE AIR NAVIGATION SYSTEM FANS SUPPORT

THIS CONTRACT IS FOR THE DESIGN AND FABRICATION OF RADIATION HARDENED CHIPLET DEVICES

FUELEAP (FOSTERING ULTRA-EFFICIENT, LOW-EMITTING AVIATION POWER) POWER SYSTEM DESIGN, ANALYSIS, AND TESTING THE SCOPE OF THIS TASK ORDER IS TO DEVELOP ENGINEERING DATA TO SUPPORT THE DESIGN AND DEVELOPMENT OF A HEAVY-FUEL, HYBRID-ELECTRIC SOFC POWER SYSTEM (SOFC POWER SYSTEM) FOR AN AIRBORNE FLIGHT DEMONSTRATOR. THIS INCLUDES IDENTIFYING SYSTEM-LEVEL TRADEOFFS, IDENTIFYING PERFORMANCE, COST AND RISK OF DESIGN ALTERNATIVES, SELECTING COMPONENTS, AND QUANTIFYING SYSTEM PERFORMANCE THROUGH INTEGRATED ANALYSIS AND TESTING. THIS TASK ORDER SHALL GENERATE PRELIMINARY DESIGN DATA, TEST PLANS, AND SHALL EXECUTE COMPONENT-LEVEL AND INTEGRATED TESTED FOR SELECTED HIGH-RISK COMPONENTS, INCLUDING THE SOFC STACK AND FUEL REFORM

DFM SIMULATION THE SCOPE OF THIS TASK ORDER IS TO UPGRADE THE CAPABILITIES OF AN AFP PSS PACKAGE SO THAT IT BETTER INFORMS THE PART DESIGNER AND ANALYST OF MANUFACTURING CONSTRAINTS AND IMPACTS OF DESIGN DECISIONS ON PART PERFORMANCE AND QUALITY. THE CONTRACTOR SHALL VALIDATE THESE NEW SOFTWARE CAPABILITIES AS PART OF THIS TASK ORDER. THE UPGRADED SOFTWARE WILL ALLOW NASA TO BETTER DESIGN AND ANALYZE COMPOSITE PARTS MADE ON THE INTEGRATED STRUCTURAL ASSEMBLY OF ADVANCED COMPOSITES ISAAC AFP SYSTEM IN SUPPORT OF THE ACP AND OTHER NASA PROJECTS.

THE ADVANCED TECHNOLOGY SUPPORT PROGRAM (ATSP) CONTRACT ACQUIRES PROGRESSIVE MICROELECTRONIC CAPABILITY SOLUTIONS FOR THE SEA SWARMING PLATFORMS FOR INSTRUMENTATION AND DESTRUCT RELAY (SEASPIDR) WIDOW 2.0 SYSTEM.

BOEING SHALL PROVIDE SUPERSONIC INLET BLEED EXPERIMENTS OF CURVED SURFACES FOR COMPUTATIONAL FLUID DYNAMICS MODELING WITH THE SUPPORT OF NC STATE UNIVERSITY RESEARCH TEAM.

FORSEE

MMRS ANNUAL MAINTENANCE RENEWAL AND SOFTWARE UPGRADE

ATSP4 FULL& OPEN PERFORMANCE WORK STATEMENTVISION STATEMENTTHE DEFENSE MICROELECTRONICS ACTIVITY (DMEA) ATSP4 IS A UNIFORM TECHNICAL AND MANAGEMENT APPROACH THAT LEVERAGES ADVANCED TECHNOLOGIES TO MEET THE REQUIREMENTS OF THE DEPARTMENT OF DEFENS

THE ADVANCED TECHNOLOGY SUPPORT PROGRAM (ATSP) CONTRACT ACQUIRES PROGRESSIVE MICROELECTRONIC CAPABILITY SOLUTIONS FOR THE AN/ALE-47 SYSTEM AS INSTALLED ON THE P-8A POSEIDON AIRCRAFT.