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This title is printed to order. This book may have been self-published. If so, we cannot guarantee the quality of the content. In the main most books will have gone through the editing process however some may not. We therefore suggest that you be aware of this before ordering this book. If in doubt check either the author or publisher’s details as we are unable to accept any returns unless they are faulty. Please contact us if you have any questions.
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.
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This title is printed to order. This book may have been self-published. If so, we cannot guarantee the quality of the content. In the main most books will have gone through the editing process however some may not. We therefore suggest that you be aware of this before ordering this book. If in doubt check either the author or publisher’s details as we are unable to accept any returns unless they are faulty. Please contact us if you have any questions.
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.