Complex of devices for determining the physical and mechanical properties of the carbon materials used in the rocket and space technology by the impact indentation method

A. P. Kren; T. A. Protasenia; A. K. Arnautov; V. A. Rudnitskii

doi:10.1007/s11029-015-9493-8

Complex of devices for determining the physical and mechanical properties of the carbon materials used in the rocket and space technology by the impact indentation method

A. P. Kren^*
, T. A. Protasenia
, A. K. Arnautov
, V. A. Rudnitskii

^*Corresponding author for this work

Institute for Mechanics of Materials

Belarus Academy of Sciences

Research output: Contribution to journal › Article › peer-review

2 Citations (Scopus)

Abstract

The results of checking of the physical and mechanical characteristics of carbon materials by the dynamic indentation method are presented. It is shown that the method and the devices created allow one to control the hardness, strength, and elastic modulus of the isotropic pyrolytic graphite and carbon laminates used to manufacture articles for the rocket and space technology.

Original language	English
Article number	A009
Pages (from-to)	225-230
Number of pages	6
Journal	Mechanics of Composite Materials
Volume	51
Issue number	2
DOIs	https://doi.org/10.1007/s11029-015-9493-8
Publication status	Published - 17 May 2015

Keywords

Anisotropy
Carbon materials
Indentation
Mechanical properties

Access to Document

10.1007/s11029-015-9493-8

Cite this

@article{bc5c01bce6794aa8927d64b50e1caaa7,

title = "Complex of devices for determining the physical and mechanical properties of the carbon materials used in the rocket and space technology by the impact indentation method",

abstract = "The results of checking of the physical and mechanical characteristics of carbon materials by the dynamic indentation method are presented. It is shown that the method and the devices created allow one to control the hardness, strength, and elastic modulus of the isotropic pyrolytic graphite and carbon laminates used to manufacture articles for the rocket and space technology.",

keywords = "Anisotropy, Carbon materials, Indentation, Mechanical properties",

author = "Kren, \{A. P.\} and Protasenia, \{T. A.\} and Arnautov, \{A. K.\} and Rudnitskii, \{V. A.\}",

note = "Publisher Copyright: {\textcopyright} 2015 Springer Science+Business Media New York.",

year = "2015",

month = may,

day = "17",

doi = "10.1007/s11029-015-9493-8",

language = "English",

volume = "51",

pages = "225--230",

journal = "Mechanics of Composite Materials",

issn = "0191-5665",

publisher = "Springer New York",

number = "2",

}

Complex of devices for determining the physical and mechanical properties of the carbon materials used in the rocket and space technology by the impact indentation method. / Kren, A. P.; Protasenia, T. A.; Arnautov, A. K. et al.
In: Mechanics of Composite Materials, Vol. 51, No. 2, A009, 17.05.2015, p. 225-230.

Research output: Contribution to journal › Article › peer-review

TY - JOUR

T1 - Complex of devices for determining the physical and mechanical properties of the carbon materials used in the rocket and space technology by the impact indentation method

AU - Kren, A. P.

AU - Protasenia, T. A.

AU - Arnautov, A. K.

AU - Rudnitskii, V. A.

PY - 2015/5/17

Y1 - 2015/5/17

N2 - The results of checking of the physical and mechanical characteristics of carbon materials by the dynamic indentation method are presented. It is shown that the method and the devices created allow one to control the hardness, strength, and elastic modulus of the isotropic pyrolytic graphite and carbon laminates used to manufacture articles for the rocket and space technology.

AB - The results of checking of the physical and mechanical characteristics of carbon materials by the dynamic indentation method are presented. It is shown that the method and the devices created allow one to control the hardness, strength, and elastic modulus of the isotropic pyrolytic graphite and carbon laminates used to manufacture articles for the rocket and space technology.

KW - Anisotropy

KW - Carbon materials

KW - Indentation

KW - Mechanical properties

UR - https://www.scopus.com/pages/publications/84943201328

U2 - 10.1007/s11029-015-9493-8

DO - 10.1007/s11029-015-9493-8

M3 - Article

AN - SCOPUS:84943201328

SN - 0191-5665

VL - 51

SP - 225

EP - 230

JO - Mechanics of Composite Materials

JF - Mechanics of Composite Materials

IS - 2

M1 - A009

ER -

Complex of devices for determining the physical and mechanical properties of the carbon materials used in the rocket and space technology by the impact indentation method

Abstract

Keywords

Access to Document

Other files and links

Fingerprint

Cite this