Federal contract award
80LARC17F0001
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).
Award details
Obligations, current value and potential value describe different measures; they are never added together.
| Field | Reported value |
|---|---|
| Agency | National Aeronautics and Space Administration |
| Office | NASA LANGLEY RESEARCH CENTER |
| NAICS | 541712 |
| PSC | AR11 — SPACE R&D SERVICES; SPACE FLIGHT, RESEARCH AND SUPPORTING ACTIVITIES; BASIC RESEARCH |
| Parent award / vehicle | NNL16AA04B |
| Set-aside | Not reported |
| Pricing type | COST PLUS FIXED FEE |
| Obligations | $538.9K |
| Current contract value | $558.0K |
| Potential contract value / ceiling | $558.0K |
| Start date | Jun 19, 2017 |
| Current end date | Oct 31, 2020 |
| Potential end date | Oct 31, 2020 |
| Latest award activity | Aug 13, 2026 |
| Source loaded | Sep 26, 2026 |
Funding and modification history
Showing the latest 11 of 11 loaded transactions. Negative values are deobligations.
| Date | Modification | Obligation change | Description |
|---|---|---|---|
| Aug 13, 2026 | P00010 | $-19.2K | "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 MATERIA |
| Jul 21, 2020 | P00009 | $180.2K | "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 MATERIA |
| May 21, 2020 | P00008 | $0 | "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 MATERIA |
| Apr 29, 2020 | P00007 | $25.9K | "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). |
| Aug 26, 2019 | P00006 | $100.0K | "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). |
| Jun 27, 2019 | P00005 | $0 | "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). |
| May 6, 2019 | P00004 | $25.0K | "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). |
| Sep 5, 2018 | P00003 | $25.0K | "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). |
| Jul 3, 2018 | P00002 | $75.0K | "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). |
| Apr 27, 2018 | P00001 | $25.0K | "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). |
| Jun 19, 2017 | 0 | $102.0K | 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). |
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