Engineering topics
Publications and source records attributed to Chase, Theodore L..
Instrumentation system measures and records accelerations at frequencies from 0 to 100 Hz and magnitudes from 10 to the negative 5th power to 0.5 g. Developed to aid research on small accelerations in spacecraft in orbit. Also used on Earth: with modified acceleration sensors to monitor acceleration environments of sensitive products transported by airplanes, railroad trains, trucks, or ships.
The primary objective of the Space Acceleration Measurement Systems (SAMS) project is to provide an acceleration measurement system capable of serving a wide variety of space experiments. The design of the system being developed under this project takes into consideration requirements for experiments located in the middeck, in the orbiter bay, and in Spacelab. In addition to measuring, conditioning, and recording accelerations, the system will be capable of performing complex calculations and interactive control. The main components consist of a remote triaxial optical storage device. In operation, the triaxial sensor head produces output signals in response to acceleration inputs. These signals are preamplified, filtered and converted into digital data which is then transferred to optical memory. The system design is modular, facilitating both software and hardware upgrading as technology advances. Two complete acceleration measurement flight systems will be build and tested under this project.