Pengembangan Metoda untuk Menganalisis Struktur Nozel Roket RX-250  

Oleh:

Ginting, Salam ; Triharjanto, Robertus Heru

Jenis: Article from Journal - ilmiah nasional
Dalam koleksi: Majalah Sains dan Teknologi Dirgantara (Fulltext) vol. 1 no. 1 (Jan. 1999), page 21-30.
Topik: Struktur Nozel Roket RX-250

Ketersediaan

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

Lihat Detail Induk

Isi artikel

The structural analysis in designing the RX-250 rocket nozzle is a significant process in minimising the weight of the rocket. This paper discused the process in determining the dimension of the RX-250 rocket nozzle. The structural calculation used the input from aerothermodynamic characteristic of the nozzle, that was the pressure and temperature inside the nozzle. New methods were used on the aerothermodynamics system of the nozzle and the strength of material calculation, which define the safety factor desired at the beginning of the calculation. These methods successfully reduce the weight of the nozzle by 40%.

Opini Anda

Klik untuk menuliskan opini Anda tentang koleksi ini!

Kembali