Parametrical Analysis and Synthesis of Starting Device Mechanisms of Low-Weight Pilotless Aircrafts

Authors

  • G. S. Alenchenkov Kalashnikov Izhevsk State Technical University
  • A. E. Pushkarev Kalashnikov Izhevsk State Technical University

Keywords:

parametrical analysis and synthesis of mechanisms, starting device, pilotless aircraft

Abstract

Process of starting the low-weight pilotless aircrafts from various starting devices is considered. Conditions of minimizing the shock accelerations at start are determined.

Author Biographies

G. S. Alenchenkov, Kalashnikov Izhevsk State Technical University

; Kalashnikov Izhevsk State Technical University

A. E. Pushkarev, Kalashnikov Izhevsk State Technical University

; Kalashnikov Izhevsk State Technical University

References

Аленченков Г. С., Пушкарев А. Э. Функционально-структурная модель стартовых устройств летательных аппаратов малой массы // Вестник ИжГТУ. - 2011. - № 2(50). - С. 4-7.

Пат. на полезную модель 98396 РФ, МПК B64F 1/06. Катапульта / Г. С. Аленченков, А. Э. Пушкарев. - № 2010119280/11. - Заявлено 13.05.2010. Опубл. 20.10.2010. - Бюл. № 29.

Аэродинамика автомобиля / под ред. В. Г. Гухо. - М. : Машиностроение, 1987. - 424 с.

Downloads

Published

15.06.2012

How to Cite

Alenchenkov Г. С., & Pushkarev А. Э. (2012). Parametrical Analysis and Synthesis of Starting Device Mechanisms of Low-Weight Pilotless Aircrafts. Vestnik IzhGTU Imeni M.T. Kalashnikova, (2), 4–7. Retrieved from https://izdat.istu.ru/index.php/vestnik/article/view/2117

Issue

No. 2 (2012)

Section

Articles