Research pressure instrumentation for NASA Space Shuttle main engine, modification no. 5
Abstract
Research concerning the development of pressure instrumentation for the space shuttle main engine is reported. The following specific topics were addressed: (1) transducer design and materials, (2) silicon piezoresistor characterization at cryogenic temperatures, (3) chip mounting characterization, and (4) frequency response optimization.
- Publication:
-
Monthly Progress Report Honeywell
- Pub Date:
- May 1984
- Bibcode:
- 1984hwi..reptR....A
- Keywords:
-
- Chips (Electronics);
- Frequency Response;
- Piezoelectricity;
- Pressure Sensors;
- Resistors;
- Space Shuttle Main Engine;
- Costs;
- Cryogenics;
- Optimization;
- Project Management;
- Project Planning;
- Research Management;
- Instrumentation and Photography