Osnovy Proektirovaniya Raketno-Pryamotochnyh Dvigatelej

V uchebnom posobii izlozheny termo-aerodinamicheskie osnovy proektirovaniya raketno-pryamotochnyh dvigatelej (RPD) dlya bespilotnyh letatel'nyh apparatov. Znachitel'noe vnimanie udeleno kompleksnomu proektirovaniyu RPD, vklyuchaya inzhenernye metody rascheta vyhodnyh harakteristik, i vyboru tipa topliva, a takzhe opredeleniyu optimal'nyh harakteristik letatel'nogo apparata i sistem avtomaticheskogo regulirovaniya. Predlagaemye metody rascheta optimal'nyh parametrov letatel'nogo apparata, RPD i sistem avtomaticheskogo regulirovaniya obespechivayut maksimal'nuyu dal'nost' poleta. This book, "Osnovy proektirovaniya raketno-pryamotochnyh dvigatelej", by B. V. Orlov, G. YU. Mazing, is a replication of a book originally published before 1967. It has been restored by human beings, page by page, so that you may enjoy it in a form as close to the original as possible.