Deployment Testing of Inflatable Membrane Tube
Xiaofeng Liu
Abstract
Xiaofeng Liu
Abstract
The deployment property of inflatable membrane tube was studied through experiment under various inflation rates and initial deployment angles in this paper,while the friction caused by gravity was erased by guide track efficiently.The relationships between deployment angle and time,deployment acceleration and time,and inner pressure and time respectively were obtained.The experiment result and analysis showed that the inflation and deployment process were separate,the inflation process could be treated as constant pressure process,and the pressure fluctuation at the folding place wasn't identical with the whole pressure fluctuation.
OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
The deployment property of inflatable membrane tube was studied through experiment under various inflation rates and initial deployment angles in this paper,while the friction caused by gravity was erased by guide track efficiently.The relationships between deployment angle and time,deployment acceleration and time,and inner pressure and time respectively were obtained.The experiment result and analysis showed that the inflation and deployment process were separate,the inflation process could be treated as constant pressure process,and the pressure fluctuation at the folding place wasn't identical with the whole pressure fluctuation.
Key concepts: Inflatable, Software deployment, Tube (container), Acceleration, Inflation (cosmology), Process (computing), Aerospace engineering, Simulation