Highly Concentrated Ceramic Binding Suspensions (HCBS) and Ceramic Castables. Stages in Research and Development

Highly Concentrated Ceramic Binding Suspensions (HCBS) and Ceramic Castables. Stages in Research... Refractories and Industrial Ceramics Vol. 44, No. 3, 2003 UDC 666.974.2:666.3.7 HIGHLY CONCENTRATED CERAMIC BINDING SUSPENSIONS (HCBS) AND CERAMIC CASTABLES. STAGES IN RESEARCH AND DEVELOPMENT Yu. E. Pivinskii Translated from Novye Ogneupory, No. 2, pp. 28 – 39, February, 2003. velopment of ceramic fairings for missiles of different Precisely 25 years ago, in the journal Ogneupory (Febru- classes [13 – 16]. In distinction from the early fiber glass ary, 1978), our paper “Fundamentals of ceramic castable fairings that were designed for missile velocities of up to two technology” was published [1]. Earlier, the principles out- lined in that paper were reported and discussed at All-Union Mach numbers, fairings were required for velocities reaching conferences held in 1976 in Sverdlovsk and Leningrad. ten Mach numbers. Upon firing such a missile, the missile’s Dating back to 1968, the first data on highly concentrated fairing, because of the aerodynamic drag, develops within binding suspensions based on quartz glass were reported in 2 – 5 sec a temperature exceeding 1500°C; occasionally, the [2, 3]. The technology of ceramic castables is precisely based temperature may be as high as 2500°C [13, 14]. The fairings, on the use of ceramic binding suspensions. In 1969 [4], http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Refractories and Industrial Ceramics Springer Journals

Highly Concentrated Ceramic Binding Suspensions (HCBS) and Ceramic Castables. Stages in Research and Development

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Publisher
Kluwer Academic Publishers-Plenum Publishers
Copyright
Copyright © 2003 by Plenum Publishing Corporation
Subject
Materials Science; Characterization and Evaluation of Materials; Materials Science, general; Ceramics, Glass, Composites, Natural Materials
ISSN
1083-4877
eISSN
1573-9139
D.O.I.
10.1023/A:1026300217117
Publisher site
See Article on Publisher Site

Abstract

Refractories and Industrial Ceramics Vol. 44, No. 3, 2003 UDC 666.974.2:666.3.7 HIGHLY CONCENTRATED CERAMIC BINDING SUSPENSIONS (HCBS) AND CERAMIC CASTABLES. STAGES IN RESEARCH AND DEVELOPMENT Yu. E. Pivinskii Translated from Novye Ogneupory, No. 2, pp. 28 – 39, February, 2003. velopment of ceramic fairings for missiles of different Precisely 25 years ago, in the journal Ogneupory (Febru- classes [13 – 16]. In distinction from the early fiber glass ary, 1978), our paper “Fundamentals of ceramic castable fairings that were designed for missile velocities of up to two technology” was published [1]. Earlier, the principles out- lined in that paper were reported and discussed at All-Union Mach numbers, fairings were required for velocities reaching conferences held in 1976 in Sverdlovsk and Leningrad. ten Mach numbers. Upon firing such a missile, the missile’s Dating back to 1968, the first data on highly concentrated fairing, because of the aerodynamic drag, develops within binding suspensions based on quartz glass were reported in 2 – 5 sec a temperature exceeding 1500°C; occasionally, the [2, 3]. The technology of ceramic castables is precisely based temperature may be as high as 2500°C [13, 14]. The fairings, on the use of ceramic binding suspensions. In 1969 [4],

Journal

Refractories and Industrial CeramicsSpringer Journals

Published: Oct 17, 2004

References

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