Research and Development for Reducing the Shock Environment for Space Transportation Systems

Hiroshi IKAIDA,Keita TERASHIMA,Toru KAMITA

Supēsu, Enjiniaringu, Konfarensu kōen rombunshū/Supesu, Enjiniaringu, Konfarensu koen ronbunshu（2020）

Cited 0|Views1

Abstract

This paper describes the design, analysis and flight results of the low-shock separation mechanism for payload adapter. The low-shock separation mechanism is based on a simple four-bar linkage, which makes the release speed of the clamp band tension lower than the current pyrotechnics system. In this paper, we describe the result of development, flight demonstration with using dummy payload ring and flight with actual satellite.

Translated text

求助PDF

上传PDF

Bibtex

AI Read Science

AI Summary

AI Summary is the key point extracted automatically understanding the full text of the paper, including the background, methods, results, conclusions, icons and other key content, so that you can get the outline of the paper at a glance.

Example

Background

Key content

Introduction

Methods

Results

Related work

Fund

Key content

Pretraining has recently greatly promoted the development of natural language processing (NLP)
We show that M6 outperforms the baselines in multimodal downstream tasks, and the large M6 with 10 parameters can reach a better performance
We propose a method called M6 that is able to process information of multiple modalities and perform both single-modal and cross-modal understanding and generation
The model is scaled to large model with 10 billion parameters with sophisticated deployment, and the 10 -parameter M6-large is the largest pretrained model in Chinese
Experimental results show that our proposed M6 outperforms the baseline in a number of downstream tasks concerning both single modality and multiple modalities We will continue the pretraining of extremely large models by increasing data to explore the limit of its performance

Upload PDF to Generate Summary

Must-Reading Tree

Example

Generate MRT to find the research sequence of this paper

Data Disclaimer

The page data are from open Internet sources, cooperative publishers and automatic analysis results through AI technology. We do not make any commitments and guarantees for the validity, accuracy, correctness, reliability, completeness and timeliness of the page data. If you have any questions, please contact us by email: report@aminer.cn

Chat Paper

【要点】：本文介绍了用于降低太空运输系统冲击环境的低冲击分离机构的设计、分析和飞行结果，该机构采用四杆联动机制，降低了夹紧带张力的释放速度，相较于传统的爆炸系统具有显著优势。

【方法】：作者基于四杆联动原理设计了一种低冲击分离机构，通过降低释放速度，减少分离时的冲击力。

【实验】：实验部分包括使用模拟有效载荷环进行的飞行演示以及实际卫星的飞行测试，均验证了该低冲击分离机构的有效性。