RETALT_TPS design and manufacturing

Author:

Paixão SofiaORCID,Peixoto Cláudia,Reinas Marta,Carvalho João

Abstract

AbstractThe present document discusses the development of a new trowelable Thermal Protection System (TPS), able of being mixed, applied and cured directly onto the vehicle structure, with the aim to fulfill the requirements of the thermal properties for the re-usable launch vehicle studied in the Retro Propulsion Landing Technology (RETALT) project. During the development of this TPS, several formula optimizations were made to improve or eliminate cracks in the char surface, increase char stiffness, rheological adjustments, and adhesion improvement to different substrates. The most promising material developed is composed by cork and epoxy resin, together with a set of rheological and thermal resistance additives, that makes it possible to be applied with a spatula, while at the same time it is able to withstand the demanding environmental conditions during atmospheric reentry. In terms of thermal properties, the developed material has a higher thermal conductivity than the current P50 TPS commercialized by Amorim Cork Composites (ACC), but it has a better behavior when exposed to flame conditions. It is expected that the absence of cracks improves its structure and resistance to demanding conditions. The development work included a detailed study of the composition and processes required for the development of a TPS material, which were evaluated by several types of flame characterization tests and thermal properties analysis.

Funder

horizon 2020 framework programme

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference22 articles.

1. Davis, D.: Fundamentals of launch vehicle ablative thermal protection system (TPS) materials. https://ntrs.nasa.gov/citations/20170009022 (2017). Accessed 2021

2. Duffa, G.: Ablative thermal protection systems modeling, pp. 9–13. AIAA Education Series (2013)

3. Uyanna, O., Najafi, H.: Thermal protection systems for space vehicles: a review on technology development, current challenges and future prospects. Acta Astronaut. 176, 341–356 (2020)

4. Effie, G.: Thermal protection and control: internship report, pp. 1–8. University Lincoln Nebraska (2013)

5. Stackpoole, M., Ghandehari, E., Covington, J.T.M.: Flexible ablators. Patent US 9,592,923 B1, 14 March (2017)

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3