IGF::OT::IGF A TRANSDUCER ELEMENT THAT IS HEARTY ENOUGH FOR A MARS LANDER MISSION NEEDS TO BE DEVELOPED SO…
Award details are derived from public USAspending.gov records. Not a bid recommendation.
Award details
- Award ID
- NNX14CP69C
- Contractor
- Awarding agency
- National Aeronautics and Space Administration
- Sub-agency / office
- National Aeronautics and Space Administration
- Award amount
- $0
- Period of performance
- Sep 26, 2014 – Sep 25, 2016
- NAICS
- 541712 — Research and Development in the Physical, Engineering, and Life Sciences
- PSC
- PSC AR11
- Place of performance
- NC
Public award description
IGF::OT::IGF A TRANSDUCER ELEMENT THAT IS HEARTY ENOUGH FOR A MARS LANDER MISSION NEEDS TO BE DEVELOPED SO THAT A SIX-AXIS FORCE AND TORQUE TRANSDUCER IS POSSIBLE. THE TECHNICAL OBJECTIVES ARE: 1. A TRANSDUCER ELEMENT CAPABLE OF SURVIVING TEMPERATURES FROM -135C TO +125C. 2. THE TRANSDUCER ELEMENT IN OBJECTIVE 1 WITH TEMPERATURE COMPENSATION TO MINIMIZE SPAN AND OFFSET DRIFT FROM -80C TO +70C. 3. THE TRANSDUCER ELEMENT IN OBJECTIVE 2 CONSTRUCTED SO THAT IT WILL SENSE PROPERLY IN AN ATMOSPHERIC VACUUM OF 1E-5 TORR. 4. THE TRANSDUCER ELEMENT IN OBJECTIVE 3 MADE OF LOW-OUTGASSING MATERIALS THAT ARE COMPATIBLE WITH AN INTERPLANETARY SAMPLE-COLLECTING MISSION. 5. THE TRANSDUCER ELEMENT IN OBJECTIVE 4 INSTRUMENTED WITH REDUNDANT SETS OF STRAIN GAGES. IN ORDER TO ACHIEVE THE OBJECTIVES, ATI INDUSTRIAL AUTOMATION HAS DIVIDED THE PROJECT INTO THESE TASKS: * SIX DEGREE OF FREEDOM TRANSDUCER DESIGN AND FABRICATION, * LOAD FIXTURE DESIGN AND FABRICATION, * INSTRUMENTATION AND TEMPERATURE COMPENSATION OF TRANSDUCERS - USING SEMICONDUCTOR STRAIN GAGES AND - USING METAL-FOIL STRAIN GAGES, * CALIBRATION OF INSTRUMENTED BEAMS AND REDUNDANT INSTRUMENTATION, * PERFORMANCE CHARACTERIZATION OF BOTH TRANSDUCER INSTRUMENTATION TYPES AT TEMPERATURE AND VACUUM.
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