MATHEMATICAL SIMULATION OF A LARGE SIZE ROCKET MOTORS
On the basis of presented universal developed physics and mathematical model of internal chamber proc-esses a number of numerical researches concerning the analysis of particularities of the large - sized rocket motor transition to the steady - state regime was carried out. A number of significant SRM problems (such as optimization of large rocket motors start-up; gas dynamics of filling and ignition of elastic stagnation zones; ignition pressure transient in solid rockets initially filled with water and modeling of rocket motors packet transitions to the steady - state regime) were solved. Results of internal chamber modeling are pre¬sented, analyzed and discussed.
( 1.96 MB ) 
( 1.96 MB )
Issue: 2, 2002
Series of issue: Science
Rubric: Academic Articles: Chemistry, Physics, Mathematics, Technology
Pages: 23 — 32
Downloads: 857