caa a22 4500 475810449 CHVBK 20180406123757.0 cr unu---uuuuu 170329e20000501xx s 000 0 eng 10.1007/BF02699384 doi (NATIONALLICENCE)springer-10.1007/BF02699384 Lipanov A. Institute of Applied Mechanics, Ural Division, Russian Academy of Sciences, 426001, Izhevsk aut Analytical solution of the inverse problem of the interior ballistics of a controlled solid rocket motor [Elektronische Daten] [A. Lipanov] The inverse problem concerning the interior ballistics of a solid rocket motor is considered for the case where the pressure in the motor is a given time function. Given the pressure, the problem reduces to calculation of the temperature and cross-sectional area of the nozzle. An analytical solution of the inverse problem is obtained. It is shown that as the pressure changes, the combustion temperature also changes. It is found that the increase in the combustion temperature with an intense increase in pressure is greater than that under constant-volume conditions. Kluwer Academic/Plenum Publishers, 2000 Combustion, Explosion and Shock Waves Springer US 36/3(2000-05-01), 323-328 0010-5082 36:3<323 2000 36 10573 https://doi.org/10.1007/BF02699384 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF02699384 text/html Onlinezugriff via DOI NATIONALLICENCE 100 1- Lipanov A. Institute of Applied Mechanics, Ural Division, Russian Academy of Sciences, 426001, Izhevsk aut NATIONALLICENCE 773 0- Combustion, Explosion and Shock Waves Springer US 36/3(2000-05-01), 323-328 0010-5082 36:3<323 2000 36 10573 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer