Prototyping, designing, and testing of the Impact Enlarged Microgravity Meter
碩士 === 國立中央大學 === 光機電工程研究所 === 102 === This experiment is an important testing step of the microgravity meter development. The core concept of this micro-gravity meter development plan is to use the relationship between the momentum of mass blocks and the impulse of impact to measure the micro-gravi...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2014
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/f6zknr |
| Summary: | 碩士 === 國立中央大學 === 光機電工程研究所 === 102 === This experiment is an important testing step of the microgravity meter development. The core concept of this micro-gravity meter development plan is to use the relationship between the momentum of mass blocks and the impulse of impact to measure the micro-gravity field strength. Let the ball inside the terminal constrained tube fly back and forth， and measure the time of flight and bouncing acceleration， used to data to estimate the strength of micro-gravity field. In order to verify the completion of the development of micro-gravity meter， requires a tiny gravity environment. In this microgravity environment， not only the weight of gravity in the direction of flight to be small， in the direction perpendicular to the wall have a small component， which can relieve the interference of friction. In this Research， The core concept of the feasibility， find achieve， and verify it.We also design and build the ground functional test and calibration facilities to test and calibration microgravity meter payload.
|
|---|