For the 71st IAC A Novel Deployable Redundant Unit for Spacecraft Causality Analysis: Modelled With Existing Technology

Chiranthan Krishnappa, Suraj Ravichandra, Ananda Mukesh Tamilselvan , Pruthvi Jagadeesh Gavirangapura Krishnamurthy, Sushmith Thuluva, Rohith Soma
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Abstract

This abstract proposes a design that helps analyze the causalities experienced by a spacecraft during communication loss or any unpredicted event. The idea is to build a mini backup box akin deployable spacecraft unit, also called a Redundant Unit that gets deployed under the command of the central unit on the occurrence of any possible danger to the spacecraft. This deployed unit ensures to picture and measure the spacecraft parameters at the time of deployment and store the data within it. This unit also serves the purpose of storing the backup payload data of a spacecraft under an uncompromisable fate. This helps in learning the potential dangers for a spacecraft alongside preventing the complete loss of mission data during any causality. This paper propounds the overall design of the structure and internal architecture of the Redundant unit with all the required subsystems, and technologies involved. The deploying mechanisms, payloads of the redundant unit, and methods employed will be presented on the basis of the most common possible fates for spacecraft.

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一种用于航天器因果分析的新型可部署冗余单元:用现有技术建模
本摘要提出了一种设计,有助于分析航天器在通信中断或任何意外事件中所经历的伤亡。这个想法是建造一个类似于可部署航天器单元的小型备用箱,也称为冗余单元,在航天器发生任何可能的危险时,在中央单元的指挥下部署。该部署单元确保在部署时对航天器参数进行成像和测量,并将数据存储在其中。该单元还用于存储处于不可妥协命运下的航天器的备份有效载荷数据。这有助于了解航天器的潜在危险,同时防止在任何因果关系中完全丢失任务数据。本文提出了冗余单元的结构和内部架构的总体设计,包括所需的所有子系统和所涉及的技术。将根据航天器最常见的可能命运介绍部署机制、冗余单元的有效载荷和所采用的方法。
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