The DOI matches its Crossref record; 2 of the 2 references it cites were found in a registry or an index.
Ceramic matrix composites: a challenge in space-propulsion technology applications
Abstract
Various technology programs in Europe are concerned, besides developing reliable and rugged, low‐cost, throwaway equipment, with preparing for future reusable propulsion technologies. One of the key roles for realizing reusable engine components is the use of modern and innovative materials. One of the key technologies that concerns various engine manufacturers worldwide is the development of fiber‐reinforced ceramics—CMCs (ceramic matrix composites). The advantages for the developers are obvious–the low specific weight, the high specific strength over a large temperature range, and their great damage tolerance compared with monolithic ceramics make this material class extremely interesting as a construction material. Over the past few years, the EADS‐ST Company (formerly DASA) has, together with various partners, worked intensively on developing components for hypersonic engines and liquid rocket propulsion systems. In the year 2000, various hot‐firing tests with subscale (scale 1:5) and full‐scale nozzle extensions were conducted. In this year, a further decisive milestone was achieved in the sector of small thrusters, and long‐term tests served to demonstrate the extraordinary stability of the C/SiC material. Besides developing and testing radiation‐cooled nozzle components and small‐thruster combustion chambers, EADS‐ST worked on the preliminary development of actively cooled structures for future reusable propulsion systems. In order to get one step nearer to this objective, the development of a new fiber composite was commenced within the framework of a regionally sponsored program. The objective here is to create multidirectional (3D) textile structures combined with a cost‐effective infiltration process. Besides material and process development, the project also encompasses the development of special metal/ceramic and ceramic/ceramic joining techniques as well as studying and verifying nondestructive investigation processes for the purpose of testing components.
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Space-grade materials are carefully selected and specially engineered to endure the harsh conditions of outer space, encompassing factors such as the vacuum, radiation, temperature fluctuations, and microgravity.
“Space-grade materials are carefully selected and specially engineered to endure the harsh conditions of outer space, encompassing factors such as the vacuum, radiation, temperature fluctuations, and microgravity.”
From A comprehensive review of lunar-based manufacturing and construction (2024) · cites this paper as [113]
Regolith is abrasive.
“Due to the abrasive nature of regolith, materials should be selected or treated to minimize dust accumulation and damage [109-118].”
From A comprehensive review of lunar-based manufacturing and construction (2024) · cites this paper as [113]
Citations
Cites
Development and testing of C/SiC components for liquid rocket propulsion applications
Beyer, S., Strobel, F., & Knabe, H. (1999) · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · doi:10.2514/6.1999-2896 · Cited by 42
Self-citationHot-firing of an advanced 40 kN thrust chamber
Alting, J., Grauer, F., Hagemann, G., et al. (2001) · AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit · doi:10.2514/6.2001-3260 · Cited by 14
Flagged first, then by citations
Research works printed but not linked: 3
- J.Brandt K.Drechsler andR.Meistring “The Application of Three‐Dimensional Fibre Preforms for Aerospace Composite Structures ”Proceedings of the ESA Symposium—Space Applications of Advanced Structural Material ESTEC Noordwijk/NL 71–77 1990.
- Greil P., 1998, Technische Keramik, 2.AuflageHrsg
- G.MaierandB.Fruehauf(Daimler Benz Stuttgart) “Computed Tomography in the Automotive Industry—Experience with Industrial Applications ”International Symposium on Computerized Tomography for Industrial Applications and Image Processing in Radiology Berlin Germany March 15–17 1999.
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A comprehensive review of lunar-based manufacturing and construction
Azami, M., Kazemi, Z., Moazen, S., Dubé, M., Potvin, M.-J., & Skonieczny, K. (2024) · Progress in Aerospace Sciences · doi:10.1016/j.paerosci.2024.101045 · Cited by 57
Metadata
- Authors
- Schmidt, S., Beyer, S., Immich, H., Knabe, H., Meistring, R., & Gessler, A.
- Corresponding author
- Schmidt, Stephan
- ORCID
- Schmidt, Stephan
- Venue
- International Journal of Applied Ceramic Technology
- Publisher
- Wiley
- Published
- 2005-03
- Volume
- 2
- Issue
- 2
- Pages
- 85-96
- ISSN
- 1546-542X (ISSN-L)
- 1744-7402
- OpenAlex
- W1967836087
- Cited by
- 80
- References
- 2
- Citations by year
- 2026: 2 · 2025: 2 · 2024: 8 · 2023: 5 · 2022: 1 · 2021: 9 · 2020: 8 · 2019: 3 · 2018: 3 · 2017: 2 · 2016: 1 · 2015: 3 · 2014: 7 · 2013: 7 · 2012: 6
- FWCI
- 2.41
- Type
- journal article
- Language
- en
- Open access
- closed
- Locations
- International Journal of Applied Ceramic Technology (publishedVersion)
- Topics
- Physical Sciences › Materials Science › Ceramics and Composites › Advanced ceramic materials synthesis
- Physical Sciences › Materials Science › General Materials Science › Material Properties and Applications
- Physical Sciences › Engineering › Aerospace Engineering › Rocket and propulsion systems research
- Keywords
- ceramic matrix composites, C/SiC, reusable rocket engines, hypersonic engines, liquid rocket propulsion, hot-fire testing, infiltration, ceramic-metal joining, non-destructive testing, damage tolerance
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