Works about ROCKET engines

Results: 783

The prediction of thermal stability of self-reactive chemicals.

Published in:

Journal of Thermal Analysis & Calorimetry, 2005, v. 80, n. 1, p. 91, doi. 10.1007/s10973-005-0619-4

By:

Roduit, B.;
Borgeat, Ch.;
Berger, B.;
Folly, P.;
Alonso, B.;
Aebischer, J. N.

Publication type:

Article

Mechanical analysis on rocket propellants.

Published in:

Journal of Thermal Analysis & Calorimetry, 2003, v. 72, n. 3, p. 921, doi. 10.1023/A:1025082602232

By:

Herder, G.;
Weterings, F. P.;
de Klerk, W. P. C.

Publication type:

Article

Metallographic Preparation of Space Shuttle Reaction Control System Thruster Electron Beam Welds for Electron Backscatter Diffraction.

Published in:

2011

By:

Martinez, J;
Castner, W;
Figert, J;
Ventura, J;
Gonzalez, D

Publication type:

Abstract

Determination of Spray Droplet Size by Wavelet Analysis of Interferometric Images.

Published in:

Measurement Techniques, 2021, v. 64, n. 9, p. 718, doi. 10.1007/s11018-022-01994-w

By:

Stepanov, R. A.;
Batalov, V. G.

Publication type:

Article

Progress on Ablation of Nozzle Throat Inserts in Solid Rocket Motors.

Published in:

Fluid Dynamics, 2025, v. 60, n. 2, p. 1, doi. 10.1134/S0015462824605254

By:

Zhou, Z. T.;
Cao, T. Y.;
Li, Y. Q.;
Ji, L.

Publication type:

Article

Multiscale Simulation of Gas-Particle Flows in the Combustion Chambers of Solid-Propellant Rocket Motors.

Published in:

Fluid Dynamics, 2024, v. 59, n. 5, p. 1416, doi. 10.1134/S001546282460411X

By:

Brykov, N.;
Volkov, K.;
Emelyanov, V.;
Efremov, A.

Publication type:

Article

Numerical Analysis on Air Core Vortex Formation in Inclined Cylindrical Tanks.

Published in:

Fluid Dynamics, 2022, v. 57, n. 6, p. 865, doi. 10.1134/S0015462822100329

By:

Arjun, P.;
Joshy, P. J.;
Tide, P. S.

Publication type:

Article

基于正交试验设计的可渗透喷管参数影响规律分析.

Published in:

Journal of Ordnance Equipment Engineering, 2024, v. 45, n. 9, p. 116, doi. 10.11809/bqzbgcxb2024.09.014

By:

薛玉琴;
靳雨祺;
关奔;
王革

Publication type:

Article

高压自紧式聚酰亚胺垫片密封性能影响因素分析及结构优化.

Published in:

Fluid Machinery, 2024, v. 52, n. 6, p. 76, doi. 10.3969/j.issn.l005-0329.2024.06.010

By:

郑娱;
刘丽静;
李双喜;
刘登宇

Publication type:

Article

Experimental Research into an Innovative Green Propellant Based on Paraffin–Stearic Acid and Coal for Hybrid Rocket Engines.

Published in:

Inventions (2411-5134), 2024, v. 9, n. 2, p. 26, doi. 10.3390/inventions9020026

By:

Cican, Grigore;
Paraschiv, Alexandru;
Buturache, Adrian Nicolae;
Hapenciuc, Andrei Iaroslav;
Mitrache, Alexandru;
Frigioescu, Tiberius-Florian

Publication type:

Article

Structural Health Monitoring of Solid Rocket Motors: From Destructive Testing to Perspectives of Photonic-Based Sensing.

Published in:

Instruments (2410-390X), 2024, v. 8, n. 1, p. 16, doi. 10.3390/instruments8010016

By:

Korompili, Georgia;
Mußbach, Günter;
Riziotis, Christos

Publication type:

Article

Case study: Analysis and research on pipeline vibration of liquid oxygen kerosene of rocket engine and vibration reduction measures.

Published in:

Noise Control Engineering Journal, 2023, v. 71, n. 3, p. 152, doi. 10.3397/1/377114

By:

Su Yong;
Gong Wu-Qi

Publication type:

Article

Application of Reconstruction of Variational Iteration Method on the Laminar Flow in a Porous Cylinder with Regressing Walls.

Published in:

Mechanics & Mechanical Engineering, 2017, v. 21, n. 2, p. 379

By:

AZIMI, Mohammadreza;
HEDESH, Ali M.;
KARIMIAN, Saeed

Publication type:

Article

Numerical Investigation on Unsteady Pressure Oscillation of Gas⁃Solid Two⁃Phase Turbulent Flow.

Published in:

Transactions of Nanjing University of Aeronautics & Astronautics, 2024, v. 41, n. 3, p. 311, doi. 10.16356/j.1005⁃1120.2024.03.005

By:

YANG Yong;
ZANG Wenwen;
HAN Xingsi;
MAO Junkui

Publication type:

Article

An Experiment on Cavitating Flow in Rocket Engine Inducer.

Published in:

Transactions of Nanjing University of Aeronautics & Astronautics, 2019, v. 36, n. 2, p. 306, doi. 10.16356/j.1005-1120.2019.02.013

By:

LI Longxian;
DING Zhenxiao;
ZHOU Liang;
WU Yuzhen

Publication type:

Article

Visualization of aluminum agglomeration in metallized composite solid propellants.

Published in:

Science & Technology of Energetic Materials, 2024, v. 85, n. 5, p. 46

By:

Kotaro Matsumoto;
Akihiro Iwasaki;
Hiroto Habu

Publication type:

Article

Combustion-mode transition of a solid propellant rocket motor by nitrogen gas injection and combustion gas release.

Published in:

Science & Technology of Energetic Materials, 2022, v. 83, n. 6, p. 163

By:

Masafumi Tanaka;
Masashi Yamakami;
Taku Sakaguchi;
Shogo Bando;
Ryusuke Wada;
Takahiro Ito;
Toshihito Ito;
Yuta Kajiya

Publication type:

Article

Numerical analysis of combustion of hybrid rocket engine with Al powder added to solid fuel.

Published in:

Science & Technology of Energetic Materials, 2022, v. 83, n. 3, p. 71

By:

Kanami Aoki;
Akiyo Takahashi;
Kenichi Takahashi

Publication type:

Article

Metal powder ignition characteristics in a hybrid rocket engine chamber.

Published in:

Science & Technology of Energetic Materials, 2022, v. 83, n. 2, p. 1

By:

Yuta Yamazaki;
Akiyo Takahashi;
Kenichi Takahashi

Publication type:

Article

Metal powder ignition characteristics in a hybrid rocket engine chamber.

Published in:

Science & Technology of Energetic Materials, 2022, v. 83, n. 1, p. 1

By:

Yuta Yamazaki;
Akiyo Takahashi;
Kenichi Takahashi

Publication type:

Article

Study on maximum pressure rise with igniter mass in tubular grain rocket motor.

Published in:

Science & Technology of Energetic Materials, 2021, v. 82, n. 1, p. 1

By:

Ropia, Balesh;
Kalal, Rakesh;
Shekher, Himanshu;
Thakur, Dineshsingh G.

Publication type:

Article

Dynamic Effect Analysis of Cryogenic Solid-Lubricated Ball Bearings with Geometrical-Frictional Defects.

Published in:

Lubricants (2075-4442), 2024, v. 12, n. 3, p. 84, doi. 10.3390/lubricants12030084

By:

Zhao, Yuhao;
Chen, Zhenyi;
Zi, Yanyang;
Zhang, Mingquan;
Tang, Tao

Publication type:

Article

Simple Learning-Based Robust Nonlinear Control of an Electric Pump for Liquid-Propellant Rocket Engines.

Published in:

Electronics (2079-9292), 2023, v. 12, n. 16, p. 3527, doi. 10.3390/electronics12163527

By:

Jafari, Mohammad;
Reyhanoglu, Mahmut;
Kozhabek, Zhandos

Publication type:

Article

A Chinese BERT-Based Dual-Channel Named Entity Recognition Method for Solid Rocket Engines.

Published in:

Electronics (2079-9292), 2023, v. 12, n. 3, p. 752, doi. 10.3390/electronics12030752

By:

Zheng, Zhiqiang;
Liu, Minghao;
Weng, Zhi

Publication type:

Article

Automated Defect Analysis System for Industrial Computerized Tomography Images of Solid Rocket Motor Grains Based on YOLO-V4 Model.

Published in:

Electronics (2079-9292), 2022, v. 11, n. 19, p. 3215, doi. 10.3390/electronics11193215

By:

Dai, Junjie;
Li, Tianpeng;
Xuan, Zhaolong;
Feng, Zirui

Publication type:

Article

Guided Filter-Based Edge Detection Algorithm for ICT Images of Solid Rocket Motor Propellant.

Published in:

Electronics (2079-9292), 2022, v. 11, n. 14, p. N.PAG, doi. 10.3390/electronics11142118

By:

Dai, Junjie;
Li, Tianpeng;
Xuan, Zhaolong

Publication type:

Article

Thermal stability of n-TiB2 reinforced α-Al2O3/SiC based nanocomposite sintered at 1600˚C using TG/DTA under controlled Ar atmosphere.

Published in:

Journal of Engineering Research (2307-1877), 2021, v. 9, n. 4B, p. 396, doi. 10.36909/jer.8817

By:

Nallusamy, Tamilselvam;
S., Vijayakumar

Publication type:

Article

Diseño conceptual de un banco de pruebas estático para motores de cohetería tipo G y K.

Published in:

Revista Ciencia y Poder Aéreo, 2022, v. 17, n. 2, p. 120, doi. 10.18667/cienciaypoderaereo.737

By:

Mónico Muñoz, Luisa Fernanda;
Orduy Rodríguez, Jaime Enrique;
Rodríguez Ramírez, Andrés Felipe;
Higuera Hernández, Robinson

Publication type:

Article

Design of the Structure of a Three-stage Rocket to Transport a 200-kg Payload into a Low Earth Orbit.

Published in:

Revista Ciencia y Poder Aéreo, 2019, v. 14, n. 1, p. 166, doi. 10.18667/cienciaypoderaereo.627

By:

Ospina Contreras, Daimer;
Roldán Torres, Luis Carlos

Publication type:

Article

Transonic Flow Field Analysis of a Minimum Nozzle Length Rocket Engine.

Published in:

INCAS Bulletin, 2024, v. 16, n. 2, p. 3, doi. 10.13111/2066-8201.2024.16.2.1

By:

ABADA, Omar;
KBAB, Hakim;
HAIF, Sidali

Publication type:

Article

Numerical Analysis of a Supercritical Heat Transfer of Cryogenic Methane in Regeneratively Cooled Rocket Engine.

Published in:

INCAS Bulletin, 2024, v. 16, n. 1, p. 33, doi. 10.13111/2066-8201.2024.16.1.4

By:

DJEFFAL, Mohammed Amine;
BENAMARA, Nabil;
LAHCENE, Abdelkader;
BENOUAR, Ali;
BOULENOUAR, Abdelkader;
MERZOUG, Mohammed

Publication type:

Article

Numerical Analysis of Convergent-Divergent Angles and Operating Conditions Impact on Rocket Nozzle Performance Parameters.

Published in:

INCAS Bulletin, 2024, v. 16, n. 1, p. 3, doi. 10.13111/2066-8201.2024.16.1.1

By:

ALILI, Nabila;
KADDOURI, Khacem;
MOKADEM, Salem;
ALAMI, Ahmed

Publication type:

Article

Joint design and simulation of GOX-GCH4 combustion and cooling in an experimental water-cooled subscale rocket engine.

Published in:

INCAS Bulletin, 2023, v. 15, n. 4, p. 159, doi. 10.13111/2066-8201.2023.15.4.13

By:

MEREU, Alexandru;
ISVORANU, Dragos

Publication type:

Article

High concentration hydrogen peroxide for rocket fuel applications.

Published in:

INCAS Bulletin, 2020, v. 12, n. 3, p. 151, doi. 10.13111/2066-8201.2020.12.3.12

By:

PELIN, George;
STOICA, Cornel;
PELIN, Cristina - Elisabeta;
BALASA, Raluca

Publication type:

Article

Problems of ensuring the acceleration dynamics of aircraft during track tests at a speed of 1600 m/s.

Published in:

INCAS Bulletin, 2020, v. 12, p. 33, doi. 10.13111/2066-8201.2020.12.S.3

By:

ASTAKHOV, Sergey A.;
BIRIUKOV, Vasilii I.

Publication type:

Article

Original Romanian Research for a Rocket Engine with Multiple Combustion Chambers during 1940 - 1944.

Published in:

INCAS Bulletin, 2020, v. 12, n. 1, p. 229, doi. 10.13111/2066-8201.2020.12.1.22

By:

ZAGANESCU, Nicolae-Florin;
GHEORGHE, Constantin-Marcian;
KALMUTCHI, Peter

Publication type:

Article

Selection of temperature and power parameters for multimodular lunar jet penetrator.

Published in:

INCAS Bulletin, 2019, v. 11, p. 231, doi. 10.13111/2066-8201.2019.11.S.23

By:

ZAGOVORCHEV, Vladimir A.;
TUSHAVINA, Olga V.

Publication type:

Article

Dynamics of a cylindrical shell with a collapsing elastic base under the action of a pressure wave.

Published in:

INCAS Bulletin, 2019, v. 11, p. 25, doi. 10.13111/2066-8201.2019.11.S.3

By:

ANTUFEV, Boris A.;
EGOROVA, Olga V.;
RABINSKIY, Lev N.

Publication type:

Article

Methodical foundations of forecasting the reliability of products of aviation and rocket and space technology.

Published in:

INCAS Bulletin, 2019, v. 11, p. 41, doi. 10.13111/2066-8201.2019.11.S.5

By:

BIRYUKOV, Vasilii I.

Publication type:

Article

Liquid rocket engine performance assessment in the context of small launcher optimisation.

Published in:

INCAS Bulletin, 2019, v. 11, n. 3, p. 135, doi. 10.13111/2066-8201.2019.11.3.12

By:

ONEL, Alexandru-Iulian;
POPESCU, Oana-Iuliana;
NECULAESCU, Ana-Maria;
AFILIPOAE, Tudorel-Petronel;
CHELARU, Teodor-Viorel

Publication type:

Article

The design and performance on 200N-class bipropellant rocket engine using decomposed H2O2 and Kerosene.

Published in:

INCAS Bulletin, 2019, v. 11, n. 3, p. 99, doi. 10.13111/2066-8201.2019.11.3.9

By:

Yang-Suk LEE;
Jun Hwan JANG

Publication type:

Article

Performances Study of a Hybrid Rocket Engine.

Published in:

INCAS Bulletin, 2018, v. 10, n. 2, p. 173, doi. 10.13111/2066-8201.2018.10.2.16

By:

BUTURACHE, Adrian-Nicolae

Publication type:

Article

EXAMINING THE TECHNIQUE TO CONTROL THE STRUCTURE OF CURRENT IN VORTEX CHAMBERS BY WING VORTEX GENERATORS.

Published in:

Eastern-European Journal of Enterprise Technologies, 2018, v. 91, n. 5, p. 28, doi. 10.15587/1729-4061.2018.121962

By:

Turick, V.;
Kochin, V.;
Kochina, M.

Publication type:

Article

Theoretical stress mechanism and structural integrity of viscoelastic propellant grains with variable Poisson's ratio.

Published in:

Scientific Reports, 2025, v. 15, n. 1, p. 1, doi. 10.1038/s41598-025-99388-9

By:

Wang, Xueren;
Wang, Yanchao;
Qiang, Hongfu;
Bai, Jianfang;
Zhao, Zhipeng;
Luo, Chao

Publication type:

Article

DESIGN AND ANALYSIS OF FIRST STAGE ROCKET ENGINE USING BUTANE AND LIQUID OXYGEN.

Published in:

i-Manager's Journal on Mechanical Engineering, 2019, v. 9, n. 3, p. 32, doi. 10.26634/jme.9.3.15806

By:

MAJUMDER, SAMARPAN DEB

Publication type:

Article

Recycling.

Published in:: Bulletin of the Atomic Scientists, 1997, v. 53, n. 2, p. 7
Publication type:: Article

Performance analysis of lobed nozzle ejectors for high altitude simulation of rocket engines.

Published in:

International Journal of Modeling, Simulation & Scientific Computing, 2014, v. 5, n. 4, p. -1, doi. 10.1142/S1793962314500196

By:

Bruce Ralphin Rose, J.;
Veni Grace, J.

Publication type:

Article

Innovative thrust vectoring system with moveable jet vanes integrated with a moveable diffuser - Measurement and analysis of selected nozzle performance parameters.

Published in:

Bulletin of the Polish Academy of Sciences: Technical Sciences, 2024, v. 72, n. 2, p. 1, doi. 10.24425/bpasts.2023.148444

By:

NOCOŃ, Łukasz K.;
GRZYB, Marta;
SZMIDT, Piotr;
NOWAKOWSKI, Łukasz M.

Publication type:

Article

Effect of Using Fractals as Grain Configuration on the Performance of Solid Rocket Motors.

Published in:

Heat Transfer Engineering, 2025, v. 46, n. 9/10, p. 852, doi. 10.1080/01457632.2024.2347178

By:

Bhattacharya, Soham;
Mundhra, Raghav

Publication type:

Article

Selected Papers from the 27th National Conference on Internal Combustion Engines and Combustion (NCICEC 2022).

Published in:

Heat Transfer Engineering, 2025, v. 46, n. 9/10, p. 769, doi. 10.1080/01457632.2024.2347169

By:

Porpatham, Ekambaram;
Kanna, Parthasarathy Rajesh;
Mohamed Ilyas, Mohamed Ibrahim;
Chidambaram, Ramesh Kumar;
Rammohan, Arunachalam

Publication type:

Article