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Nozzle of RKX l00 rocket contributes 30 % to the total weight of the structure, so that allowing further research on weight reduction. An alternatiye for this is by substitution of massive graphite, which is currently used' as thermal protector in the nozzle, with thin layer of HVOF (High Velocity Oxy-Fuel) thermal spray...
Jurnal Teknologi, Vol. 20 (3) Maret 2006 : 203-208, 2006
JUTE-20-3-Sep2006-203
Artikel Jurnal  Universitas Indonesia Library