Indonesian Journal of Aerospace
Vol. 8 No. 1 Juni (2010): Jurnal Teknologi Dirgantara

SIMULASI DAN PERHITUNGAN SPIN ROKET FOLDED FIN BERDIAMETER 200 mm

Fitroh, Ahmad Jamaludin (Unknown)
Saeri (Unknown)

Article Info

Publish Date
08 Dec 2010

Abstract

One of rocket movement types is spin maneuver. The rocket rotation towards the axisymmetric axis is needed so the rocket can move straight in it’s flight line. The object of spin simulation and calculation in this work is the Rocket of LAPAN with the diameter of 200 mm. The simulation and calculation were done for 0.6, 1.0, 2.0, and 3.0 Mach of flight speed. The simulation and calculation results show that spin anddrag of fin will increase while the flight speed is increasing. The spin and drag of fin for 3.0 Mach of flight speed are 36 rps and 16.6 kg respectively

Copyrights © 2010




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Journal Info
Indonesian Journal of Aerospace
Website

Abbrev

ijoa

Publisher

Badan Riset dan Inovasi Nasional

Subject

Aerospace Engineering Astronomy

Description

Indonesian Journal of Aerospace provides a broad opportunity for the scientific and engineering community to report research results, disseminate knowledge, and exchange ideas in various fields related to aerospace science, technology, and policy. Topics suitable for publication in the IJoA include ...