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Arif Nur Hakim
Arif Nur Hakim
National Research and Innovation Agency - Indonesia
Verified email at brin.go.id
Title
Cited by
Cited by
Year
Fundamental study of supersonic combustion in pure air flow with use of shock tunnel
S Aso, AN Hakim, S Miyamoto, K Inoue, Y Tani
Acta Astronautica 57 (2-8), 384-389, 2005
582005
RANCANG BANGUN ENJIN ROKET CAIR DENGAN GAYA DORONG 1000 KGF MENGGUNAKAN PROPELAN ASAM NITRAT–KEROSEN (DESIGN OF LIQUID ROCKET ENGINE WITH 1000 KGF THRUST USING NITRIC ACID …
AN Hakim
Jurnal Teknologi Dirgantara 13 (1), 2015
72015
Thermal and Mechanical Properties of Hybrid Organoclay/Rockwool Fiber Reinforced Epoxy Composites
M Baiquni, B Soegijono, AN Hakim
Journal of Physics: Conference Series 1191 (1), 012056, 2019
62019
ANALISIS PROPULSI ENJIN ROKET CAIR RCX300H DENGAN STORABLE PROPELLANT ASAM NITRAT DAN KEROSEN
AN Hakim
LAPAN, 2011
62011
Analisa Uji Bakar Roket RCX2 Berpropelan GOX-Kerosen
AN Hakim
Prosiding Seminar Nasional Thermofluid, Yogyakarta, 2010
52010
ANALISIS KINERJA ENJIN ROKET CAIR ECX1000H2-3 (PERFORMANCE ANALYSIS OF LIQUID ROCKET ENGINE ECX1000H2-3)
AN Hakim, H Tahdi, T Rochman, LPDA Nasional
DAFTAR ISI, 9, 2018
32018
An experimental study of supersonic combustion with incoming high temperature pure air stream obtained by shock tunnel
AN Hakim, S Aso, S Miyamoto, K Toshimitsu
Shock Waves, 959-963, 2005
32005
Development of Supporting Technology for Sustainable Spaceport Development.
G Widiyasmoko, D Martono, H Herdiansyah, N Hakim
International Journal of Sustainable Development & Planning 18 (6), 2023
22023
Investigasi Numerik dan Peningkatan Kinerja Elemen Injektor Enjin Roket Cair ECX1000H2-2
AN Hakim
Prosiding SIPTEKGAN XXI-2017 Seminar Nasional Iptek Penerbangan & Antariksa …, 2017
22017
Investigasi Aliran Fluida Pada Elemen Injektor Berbasis Pusaran Untuk Enjin Roket Cair
AN Hakim
Bunga Rampai Hasil Litbangyasa: Teknologi Pada Pesawat Terbang, Roket, dan …, 2015
22015
Aerodynamic design of impulse turbine for liquid rocket turbopump RCX2000H1
T Rochman, AN Hakim
Aeronautics and Space Technology Research and Engineering of Unmanned Aerial …, 2015
22015
RANCANG BANGUN TABUNG KOMPOSIT TEKANAN TINGGI UNTUK PROPELAN ROKET CAIR KOROSIF (DESIGN OF COMPOSITE OVERWRAPPED PRESSURE VESSEL FOR CORROSIVE LIQUID ROCKET PROPELLANT)
AN Hakim, P Sitinjak, T Rochman
Jurnal Teknologi Dirgantara 13 (2), 2015
22015
Desain Nosel Roket Cair RCX250 Menggunakan Metode Parabolik dengan Modifikasi Sudut Ekspansi
E Priamadi, AN Hakim, RO Bura
Jurnal Teknologi Dirgantara 9 (1), 2011
22011
Experimental study on effects of shock wave impingement on supersonic combustion
AN Hakim, S Aso, Y Tani
Memoirs of the Faculty of Engineering, Kyushu University, Japan 68 (1), 2008
22008
Modeling and simulation of a canard-based sounding rocket dynamics at climb and descent phases
A Hanif, IE Putro, RA Duhri, H Hakiki, AN Hakim, L Mariani, R Andiarti, ...
AIP Conference Proceedings 2941 (1), 2023
12023
Implementation of Simple Throttling for Liquid Rocket Engine ECX1000H2-4
AN Hakim, H Tahdi, FL Mahendra
2020 6th International Conference on Science and Technology (ICST) 1, 1-5, 2020
12020
Model Predictive Control in Hardware in the Loop Simulation for the OnBoard Attitude Determination Control System
HY Irwanto, P Yusgiantoro, ZA Sahabuddin, RO Bura, E Artono, ...
Journal of Robotics and Control (JRC) 5 (2), 533-541, 2024
2024
Morphological and mechanical studies of Al 2 O 3–Na 2 SiO 3 as a skin barrier coated with TiO 2 for carbon fiber reinforced composite materials
S Hardiyanti, WSM Al Haq, LL Zulfa, N Safrida, AN Hakim, L Mariani, ...
RSC Advances 14 (14), 9483-9496, 2024
2024
Low Reflection-Loss Thermal Barrier Coating on Hastelloy C276 for Radio Control Rocket Tip Nosecone Using Yttria-Stabilized Zirconia (YSZ) at Extreme Temperature
W Widyastuti, RA Wahyuono, R Fajarin, S Sulistijono, AN Hakim, ...
Solid State Phenomena 354, 49-60, 2023
2023
Thrust optimization in the trajectory control strategy for ballistic rocket
IH Yudhi, Y Purnomo, SZ Abidin, BR Oktovianus, N Arif, PI Eko, S Aris, ...
AIP Conference Proceedings 2941 (1), 2023
2023
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