Mining computer program development of system "housing – filling compound" strength design analysis of space launchers solid propellant engines

1Satokin, VV, 1Kharchenko, VN, 1Tonkonozhenko, AM, 1Gamaza, EA
1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2002, 8 ;(Supplement1):049-051
https://doi.org/10.15407/knit2002.01s.049
Publication Language: Російська
Abstract: 
The article present the results of development of the computer program for the calculation of mechanical condition of firmly cemented system "housing—filling compound" of solid propellant engines for space launchers. The program is based on the engineering techniques created on the basis of theoretical and experimental investigation tried-out in the process of test of full-scale design of solid-propellant engines and is made in the programming system Delphi.
References: 
1. Arkhangelsky A. Ya. Delphi 4 Programming. (Nauka, Moscow, 1999) [in Russian].
2. Ilyushin A. A., Pobedrya B. E. Foundations of mathematical theory of thermoviscoelasticity. (Nauka, Moscow, 1970) [in Russian].

3. Fakhrutdinov I. H. Rocket engines solid fuel. (Nauka, Moscow, 1970) [in Russian].