Analisa Karakteristik Aerodinamika Roket Balistik Penjaga Selat  

Oleh:

Ginting, Salam

Jenis: Article from Journal - ilmiah nasional
Dalam koleksi: Majalah Sains dan Teknologi Dirgantara (Fulltext) vol. 1 no. 1 (Jan. 1999), page 7-20.
Topik: Aerodinamika Roket Balistik; Penjaga Selat; koefisien aerodinamik

Ketersediaan

Perpustakaan Pusat (Semanggi) Nomor Panggil: MM32.1 Non-tandon: 1 (dapat dipinjam: 0) Tandon: tidak ada

Lihat Detail Induk

Isi artikel

This paper presents the analysis on the aerodynamic characteristics of a 150 mm diameter ballistic rocket. The rocket is intended to be used in a tactical strait defense. The methods used in the analysis are thostly from the N.F. Krasnov aerodynamic theory since the book focuses on the specific rocket technology. The obtained aerodynamic characteristics are shown in the form of lift, drag, and momen curves. The aerodynamic coefficient data was used as an input to predict the static stability of the rocket in subsonic and supersonic speed. The data also used in designing the rocket trajectory and range, so that the rocket will be effective as a weapon in defending strait. As a comparison and to validate the calculation, the data from similar rocket which has been tested in Indonesia and abroad are also presented.

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