Design, development and flight performances of deceleration system

Paul Johns; Aggarwal Atin; Nalluveettil Santhosh J.; Purushothaman P.; Premdas M.

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Design, development and flight performances of deceleration system

机译：减速系统的设计，开发和飞行性能

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Human Spaceflight Programme (HSP) of Indian Space Research Organisation is proposed with the objective of carrying two crew members to low Earth orbit and bring them back safely to a predetermined location on Earth. The deceleration system for the programme has been designed for a 4-tonne class payload and shall cater to the requirements of nominal as well as abort missions. In order to finalize the parachute configurations and deployment sequence, detailed studies and development tests, starting from wind tunnel tests to full-scale air-drop tests were carried out. After successful structural and functional qualification of the parachutes and the various subsystems, the system was used to safely recover the module in the Crew Module Atmospheric Re-entry Experiment, the first unmanned spaceflight of HSP. This article provides details on the system configurations, deployment sequence and numerous tests that have been carried out till now in order to make the system worthy of manned flights in future.

机译：印度空间研究组织（Indian Space Research Organization，简称HSP）的人类太空飞行计划（Human Spaceflight Program，简称HSP）旨在将两名宇航员送入近地轨道，并将他们安全带回地球上预定的位置。该项目的减速系统设计用于4吨级有效载荷，并应满足标称任务和中止任务的要求。为了确定降落伞的配置和展开顺序，进行了从风洞试验到全尺寸空投试验的详细研究和开发试验。在成功确认降落伞和各子系统的结构和功能后，该系统被用于在乘员舱大气再入实验中安全回收该舱，这是HSP的首次无人航天飞行。本文详细介绍了系统配置、部署顺序和迄今为止进行的大量测试，以使该系统值得在未来进行载人飞行。

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来源
《Current Science: A Fortnightly Journal of Research》 |2021年第1期|共7页
作者
Paul Johns; Aggarwal Atin; Nalluveettil Santhosh J.; Purushothaman P.; Premdas M.;
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作者单位

Indian Space Res Org Vikram Sarabhai Space Ctr Mech &

Vehicle Integrat Testing Ent Aerosp Mech Grp Thiruvananthapuram 695547 Kerala India;

Indian Space Res Org Vikram Sarabhai Space Ctr Mech &

Vehicle Integrat Testing Ent Aerosp Mech Grp Thiruvananthapuram 695547 Kerala India;

Indian Space Res Org Vikram Sarabhai Space Ctr Mech &

Vehicle Integrat Testing Ent Aerosp Mech Grp Thiruvananthapuram 695547 Kerala India;

Indian Space Res Org Vikram Sarabhai Space Ctr Mech &

Vehicle Integrat Testing Ent Aerosp Mech Grp Thiruvananthapuram 695547 Kerala India;

Indian Space Res Org Vikram Sarabhai Space Ctr Mech &

Vehicle Integrat Testing Ent Aerosp Mech Grp Thiruvananthapuram 695547 Kerala India;

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原文格式 PDF
正文语种 eng
中图分类自然科学现状及发展;
关键词
Abort missions; deceleration system; deployment sequence parachutes; manned flights;

机译：中止任务;减速系统;降落伞的部署顺序;载人飞行;

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Design, development and flight performances of deceleration system

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