Cited by 80Advanced ceramic materials synthesisMaterial Properties and ApplicationsRocket and propulsion systems research

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

Schmidt, Stephan, Beyer, Steffen, Immich, Hans, Knabe, Helmut, Meistring, Rolf, Gessler, Andreas·2005·International Journal of Applied Ceramic Technology

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.

Overview

Integrity signals

Registry

Crossref · 10.1111/j.1744-7402.2005.02010.x

Cites

2 of 2 references verified0 citation errors · 0 not checkable

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Claims the paper makes

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Claims other papers make about this one

Each is checked against this paper’s own text: does it say what the citing paper says it does?

  • 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.”
  • Regolith is abrasive.

    “Due to the abrasive nature of regolith, materials should be selected or treated to minimize dust accumulation and damage [109-118].”

Citations

Cites

Flagged first, then by citations

Research works printed but not linked: 3

  1. 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.
  2. Greil P., 1998, Technische Keramik, 2.AuflageHrsg
  3. 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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Metadata

Authors
Schmidt, S., Beyer, S., Immich, H., Knabe, H., Meistring, R., & Gessler, A.
Corresponding author
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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