NNL13AC08TTASK ORDER statement of WORK SOW — Boeing Company, the

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TASK ORDER STATEMENT OF WORK SOW TASK TITLE BOEING LCAT ARC JET TEST IN SUPPORT OF FLEXIBLE TPS EVALUATION AND DEVELOPMENT INTRODUCTION BACKGROUND THE HYPERSONIC INFLATABLE AERODYNAMIC DECELERATOR HIAD PROJECT IS A TECHNOLOGY DEVELOPMENT EFFORT INVESTIGATING THE VIABILITY AND SURVIVABILITY OF INFLATABLE AERODYNAMIC DECELERATORS AT FLIGHT RELEVANT ENVIRONMENTS FOR APPLICATION TO FUTURE PLANETARY ENTRY SPACECRAFT IN ORDER TO EVALUATE A FLEXIBLE THERMAL PROTECTION SYSTEMS FTPS WHICH IS THE HEAT SHIELD FOR THE HIAD THE FTPS MUST BE SUBJECTED TO FLIGHT RELEVANT HEATING PRESSURES AND SHEARING ENVIRONMENTS EXPERIENCED DURING REENTRY AND SHOW MARGINED PERFORMANCE AND SURVIVAL IN SUPPORT OF THE HIAD PROJECTS FLEXIBLE SYSTEMS TECHNICAL DEVELOPMENT AREA THE NASA LANGLEY RESEARCH CENTER LARC ENGINEERING GROUP IS MODELING TESTING AND VERIFYING MODELING OF FTPS LAYUPS IN FLIGHT RELEVANT REACTIVE FLOW ENVIRONMENTS IN ORDER TO ESTABLISH A MODELING PARADIGM AND A MORE EFFECTIVE MARGIN POLICY FOR INFLATABLE AND RIGID REENTRY SYSTEMS SPECIFIC NASA PROVIDED SPECIMENS MADE UP OF VARIOUS LAYUP COMBINATIONS OF ADVANCED FLEXIBLE MATERIALS ARE MODELED AND TESTED IN FLIGHT RELEVANT CONDITIONS FOR MODEL VERIFICATION AND MARGIN MATURATION THIS EFFORT BUILDS UPON TESTING ALREADY CONDUCTED AT THE LCAT UNDER BOEINGS SMAAART CONTRACT NNL10AA05B TASK ORDER NNL11AD16T ENTITLED BOEING LCAT ARC JET TEST IN SUPPORT OF FLEXIBLE TPS EVALUATION AND DEVELOPMENT UNDER NNL11AD16T HUNDREDS OF FTPS SAMPLES HAVE BEEN EVALUATED AT SEVERAL CONDITIONS OF DEVELOPMENT INTEREST ESTABLISHING A BASIS FOR THE CRITICAL ADVANCEMENT OF THE SUCCESSFUL FLIGHT OF THE INFLATABLE REENTRY VEHICLE EXPERIMENT IRVE 3 IN JULY 2012 AND ADVANCING THE DEVELOPMENT OF THE NEXT GENERATION OF FTPS THE TESTING DESCRIBED BY THIS SOW WILL CONTINUE THIS CRUCIAL ADVANCEMENT BY BUILDING UPON THE DATABASE OF RESULTS ALREADY OBTAINED FURTHER TESTING IS NEEDED TO COMPARE MORE ADVANCED MATERIALS AND LAYUPS WITH PREVIOUSLY TESTED COUPONS AND TO EXTEND THE HEAT FLUX AND PRESSURE TEST RANGE SIMULATING HARSHER ATMOSPHERIC REENTRY FLIGHT ENVIRONMENTS SCOPE OBJECTIVES THE SCOPE OF THIS TASK ORDER IS TO EVALUATE FTPS LAYUPS AND MATERIALS AT COMPARABLE OR HARSHER SIMULATED ATMOSPHERIC REENTRY FLIGHT CONDITIONS AND RIGID DEPLOYABLE TPS LAYUPS AND MATERIALS AT MUCH HARSHER SIMULATED ATMOSPHERIC REENTRY FLIGHT CONDITIONS FTPS MATERIALS AND SYSTEMS WILL BE TESTED UTILIZING THE LCAT FACILITY FOR 12 WEEKS OF TOTAL TEST TIME AT FOUR SPECIFIC TEST CONDITIONS WHICH SIMULATE RELEVANT TEST ENVIRONMENTS THE FIRST TWO TEST CONDITIONS GIVEN IN OBJECTIVES 1 AND 2 BELOW WERE DEVELOPED UNDER TASK ORDER NNL11AD16T NEW MATERIALS AND SYSTEMS WILL BE COMPARED AT THESE CONDITIONS THE REMAINING TWO TEST CONDITIONS ARE NEW TEST REQUIREMENTS OUTLINED IN OBJECTIVES 3 AND 4 BELOW TO EXTEND THE RANGE OF THE CURRENT MATERIALS AND SYSTEMS DATA BASE THE OBJECTIVES OF THIS TASK 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 W CM2HEAT FLUX 50 W CM2 PRESSURE 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 W CM2 HEAT FLUX 75W CM2 PRESSURE 10KPA OBJECTIVE FOUR EVALUATION OF FTPS LAYUPS AND MATERIALS AT FLIGHT LIKE CONDITIONS SIMULATING A HEAT FLUX ENTRY CONDITION SQUARE PULSE IN STAGNATION OF 130 W CM2 HEAT FLUX 130 W CM2 PRESSURE BETWEEN 6 AND 12K is a federal award for Nasa Langley Research Center held by Boeing Company, the. Estimated value $1M ($-6,926.77 obligated). Current period of performance ends Oct 12, 2016. Last award drew 1 bidder. Place of performance: HUNTINGTON BEACH CA.

TASK ORDER STATEMENT OF WORK SOW TASK TITLE BOEING LCAT ARC JET TEST IN SUPPORT OF FLEXIBLE TPS EVALUATION AND DEVELOPMENT INTRODUCTION BACKGROUND THE HYPERSONIC INFLATABLE AERODYNAMIC DECELERATOR HIAD PROJECT IS A TECHNOLOGY DEVELOPMENT EFFORT INVESTIGATING THE VIABILITY AND SURVIVABILITY OF INFLATABLE AERODYNAMIC DECELERATORS AT FLIGHT RELEVANT ENVIRONMENTS FOR APPLICATION TO FUTURE PLANETARY ENTRY SPACECRAFT IN ORDER TO EVALUATE A FLEXIBLE THERMAL PROTECTION SYSTEMS FTPS WHICH IS THE HEAT SHIELD FOR THE HIAD THE FTPS MUST BE SUBJECTED TO FLIGHT RELEVANT HEATING PRESSURES AND SHEARING ENVIRONMENTS EXPERIENCED DURING REENTRY AND SHOW MARGINED PERFORMANCE AND SURVIVAL IN SUPPORT OF THE HIAD PROJECTS FLEXIBLE SYSTEMS TECHNICAL DEVELOPMENT AREA THE NASA LANGLEY RESEARCH CENTER LARC ENGINEERING GROUP IS MODELING TESTING AND VERIFYING MODELING OF FTPS LAYUPS IN FLIGHT RELEVANT REACTIVE FLOW ENVIRONMENTS IN ORDER TO ESTABLISH A MODELING PARADIGM AND A MORE EFFECTIVE MARGIN POLICY FOR INFLATABLE AND RIGID REENTRY SYSTEMS SPECIFIC NASA PROVIDED SPECIMENS MADE UP OF VARIOUS LAYUP COMBINATIONS OF ADVANCED FLEXIBLE MATERIALS ARE MODELED AND TESTED IN FLIGHT RELEVANT CONDITIONS FOR MODEL VERIFICATION AND MARGIN MATURATION THIS EFFORT BUILDS UPON TESTING ALREADY CONDUCTED AT THE LCAT UNDER BOEINGS SMAAART CONTRACT NNL10AA05B TASK ORDER NNL11AD16T ENTITLED BOEING LCAT ARC JET TEST IN SUPPORT OF FLEXIBLE TPS EVALUATION AND DEVELOPMENT UNDER NNL11AD16T HUNDREDS OF FTPS SAMPLES HAVE BEEN EVALUATED AT SEVERAL CONDITIONS OF DEVELOPMENT INTEREST ESTABLISHING A BASIS FOR THE CRITICAL ADVANCEMENT OF THE SUCCESSFUL FLIGHT OF THE INFLATABLE REENTRY VEHICLE EXPERIMENT IRVE 3 IN JULY 2012 AND ADVANCING THE DEVELOPMENT OF THE NEXT GENERATION OF FTPS THE TESTING DESCRIBED BY THIS SOW WILL CONTINUE THIS CRUCIAL ADVANCEMENT BY BUILDING UPON THE DATABASE OF RESULTS ALREADY OBTAINED FURTHER TESTING IS NEEDED TO COMPARE MORE ADVANCED MATERIALS AND LAYUPS WITH PREVIOUSLY TESTED COUPONS AND TO EXTEND THE HEAT FLUX AND PRESSURE TEST RANGE SIMULATING HARSHER ATMOSPHERIC REENTRY FLIGHT ENVIRONMENTS SCOPE OBJECTIVES THE SCOPE OF THIS TASK ORDER IS TO EVALUATE FTPS LAYUPS AND MATERIALS AT COMPARABLE OR HARSHER SIMULATED ATMOSPHERIC REENTRY FLIGHT CONDITIONS AND RIGID DEPLOYABLE TPS LAYUPS AND MATERIALS AT MUCH HARSHER SIMULATED ATMOSPHERIC REENTRY FLIGHT CONDITIONS FTPS MATERIALS AND SYSTEMS WILL BE TESTED UTILIZING THE LCAT FACILITY FOR 12 WEEKS OF TOTAL TEST TIME AT FOUR SPECIFIC TEST CONDITIONS WHICH SIMULATE RELEVANT TEST ENVIRONMENTS THE FIRST TWO TEST CONDITIONS GIVEN IN OBJECTIVES 1 AND 2 BELOW WERE DEVELOPED UNDER TASK ORDER NNL11AD16T NEW MATERIALS AND SYSTEMS WILL BE COMPARED AT THESE CONDITIONS THE REMAINING TWO TEST CONDITIONS ARE NEW TEST REQUIREMENTS OUTLINED IN OBJECTIVES 3 AND 4 BELOW TO EXTEND THE RANGE OF THE CURRENT MATERIALS AND SYSTEMS DATA BASE THE OBJECTIVES OF THIS TASK 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 W CM2HEAT FLUX 50 W CM2 PRESSURE 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 W CM2 HEAT FLUX 75W CM2 PRESSURE 10KPA OBJECTIVE FOUR EVALUATION OF FTPS LAYUPS AND MATERIALS AT FLIGHT LIKE CONDITIONS SIMULATING A HEAT FLUX ENTRY CONDITION SQUARE PULSE IN STAGNATION OF 130 W CM2 HEAT FLUX 130 W CM2 PRESSURE BETWEEN 6 AND 12K

Current PoP ended Oct 12, 2016 (3600 days ago). The usual 12–18 month agency planning window is closed — recompete action looks late / overdue relative to a normal cycle. Watch for bridge orders, follow-ons, or a new solicitation.

Boeing Company, the — $219 obligated across 7 awards (firm-wide, all agencies).