DYNAMIC ANALYSIS OF SATELLITE SEPARATION USING RETRO ROCKET FOR INJECTION WITH INITIAL ROTATION IN ORBIT

This paper presents the new method for separation of payload from launch vehicle. In this method, in addition to helical compression spring mechanism used in usual separation systems, two retro rockets mounted symmetrically on the second stage were used. To protect on-going stage from disturbance, t...

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Detalhes bibliográficos

Principais autores:	S. Sarkheil, S.E. Gardounzade, A.A. Hasibi Taheri, M. Darande
Formato:	Artigo
Idioma:	Persa
Publicado em:	Semnan University 2014-05-01
Colecção:	مجله مدل سازی در مهندسی
Assuntos:	launch vehicle payload separation retro rocket spent body separation dynamics
Acesso em linha:	https://modelling.semnan.ac.ir/article_1662_16813e35b122d957ac86dae09776ae2e.pdf
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