Works matching DE "SOLID propellant rockets"

Results: 69

COMPARATIVE STUDY OF AN ADDITIONAL OXIDIZER CHARGE EFFECT ON SELECTED OPERATIONAL CHARACTERISTICS OF A SOLID-FUEL ROCKET ENGINE.

Published in:

Technical Transactions / Czasopismo Techniczne, 2016, v. 4-M, p. 65, doi. 10.4467/2353737XCT.16.234.5983

By:

PIETRASZEK, MARIUSZ;
KLEMBA, TOMASZ;
LUBIENIECKA, JOANNA;
ŁUKASIEWICZ, JERZY;
PIETRASZEK, JACEK

Publication type:

Article

Solid-propellant gas generators with a gas flow rate stabilization system.

Published in:

Doklady Chemistry, 2015, v. 463, n. 1, p. 189, doi. 10.1134/S0012500815070022

By:

Rashkovskii, S.;
Milekhin, Yu.;
Fedorychev, A.

Publication type:

Article

SOLID ROCKET MOTOR STAR GRAIN GEOMETRICAL ANALYSIS AND PERFORMANCE MODEL.

Published in:

Annals of the Faculty of Engineering Hunedoara - International Journal of Engineering, 2020, n. 4, p. 193

By:

IONEL, Alexandru

Publication type:

Article

Solid Rocket Grain Geometry Modifications for Axial Combustion Instability Symptom Suppression.

Published in:

International Review of Aerospace Engineering, 2010, v. 3, n. 2, p. 102

By:

Greatrix, D. R.;
Baczynski, C.

Publication type:

Article

MISIONES DE COHETERÍA EXPERIMENTAL CON PROPELENTE SÓLIDO: MISIÓN SÉNECA, COHETE AINKAA 1.

Published in:

Ciencia e Ingenieria Neogranadina, 2010, v. 20, n. 2, p. 53

By:

Peña, José Alejandro Urrego;
Mora, Fabio Arturo Rojas

Publication type:

Article

A parallel solution-adaptive scheme for multi-phase core flows in solid propellant rocket motors.

Published in:

International Journal of Computational Fluid Dynamics, 2005, v. 19, n. 2, p. 159, doi. 10.1080/10618560410001729135

By:

Sachdev, J. S.;
Groth, C. P. T.;
Gottlieb, J.J.

Publication type:

Article

Investigation of high rate mechanical flow followed by ignition for high-energy propellant under dynamic extrusion loading.

Published in:

Defence Technology, 2024, v. 32, p. 336, doi. 10.1016/j.dt.2023.05.009

By:

Liying Dong;
Yanqing Wu;
Kun Yang;
Xiao Hou

Publication type:

Article

Damage-ignition mechanism studies on modified propellant with different crosslinking density under dynamic loading.

Published in:

Defence Technology, 2023, v. 28, p. 155, doi. 10.1016/j.dt.2022.08.006

By:

Hong-zheng Duan;
Yan-qing Wu;
Xiao Hou;
Kun Yang;
Feng-lei Huang

Publication type:

Article

Numerical Study on the Solid Fuel Rocket Scramjet Combustor with Cavity.

Published in:

Energies (19961073), 2019, v. 12, n. 7, p. 1235, doi. 10.3390/en12071235

By:

Li, Chaolong;
Xia, Zhixun;
Ma, Likun;
Zhao, Xiang;
Chen, Binbin

Publication type:

Article

Scale Effects on Solid Rocket Combustion Instability Behaviour.

Published in:

Energies (19961073), 2011, v. 4, n. 1, p. 90, doi. 10.3390/en4010090

By:

Greatrix, David R.

Publication type:

Article

SEM, WAXD AND ED(P)XRFS INVESTIGATIONS ON NEW SORTS OF COKE.

Published in:

Metalurgia, 2009, v. 61, n. 5, p. 45

By:

Pencea, I.;
Barca, F.;
Sfat, C. E.;
Ghiban, Brânduşa

Publication type:

Article

Successful plant scale production of solid propellant recycling from obsolete ammunition.

Published in:

Journal of Material Cycles & Waste Management, 2017, v. 19, n. 2, p. 898, doi. 10.1007/s10163-016-0495-y

By:

Shim, Yong-Ho;
Kim, Ji-Tae

Publication type:

Article

Investigation of the Ablative Properties of an EPDM\Kevlar Insulator in a Solid Rocket Motor.

Published in:

Propellants, Explosives, Pyrotechnics, 2022, v. 47, n. 1, p. 1, doi. 10.1002/prep.202100051

By:

Sapozhnikov, Igor;
Leitner, Amiram;
Natan, Benveniste;
Mograbi, Elaad

Publication type:

Article

Thermal Safety of a Gun‐Launched Missile's Solid Rocket Motor Under Conditions of High Environm. Temp. and Overloaded Forces.

Published in:

Propellants, Explosives, Pyrotechnics, 2018, v. 43, n. 12, p. 1277, doi. 10.1002/prep.201800050

By:

Ma, Weihua;
Wang, Ningfei;
Sui, Xin;
Li, Shipeng;
Xie, Kan

Publication type:

Article

Thermokinetic Analysis and Performance Evaluation of Guanidinium Azotetrazolate Based Gas Generating Composition for Testing of Solid Rocket Motor Nozzle Closures.

Published in:

Propellants, Explosives, Pyrotechnics, 2018, v. 43, n. 10, p. 1006, doi. 10.1002/prep.201800103

By:

Harikrishnan, Erezhath Shani;
Hariharanath, Bodagala;
Vineeth, Gayathri Muraleedharanpillai;
Purushothaman, Pokkan

Publication type:

Article

Comparative Study on Infrared Irradiance Emitted from Standard and Real Rocket Motor Plumes.

Published in:

Propellants, Explosives, Pyrotechnics, 2015, v. 40, n. 5, p. 779, doi. 10.1002/prep.201400213

By:

Kim, Min Taek;
Song, Soonho;
Yim, Yoo Jin;
Jang, Myung Wook;
Baek, Gookhyun

Publication type:

Article

Three-dimensional Structural Analysis Approach for Aging Composite Solid Propellant Grains.

Published in:

Propellants, Explosives, Pyrotechnics, 2014, v. 39, n. 1, p. 117, doi. 10.1002/prep.201300120

By:

Deng, Bin;
Xie, Yan;
Tang, Guo Jin

Publication type:

Article

A quasi-dynamic procedure for coupled thermal simulations.

Published in:

International Journal for Numerical Methods in Fluids, 2013, v. 72, n. 11, p. 1183, doi. 10.1002/fld.3782

By:

Errera, Marc‐Paul;
Baqué, Bénédicte

Publication type:

Article

Flow of Combustion Products Containing Condensed-Phase Particles over a Recessed Vectorable Jet Nozzle.

Published in:

Journal of Engineering Physics & Thermophysics, 2017, v. 90, n. 5, p. 1138, doi. 10.1007/s10891-017-1668-9

By:

Volkov, K.;
Denisikhin, S.;
Emel'yanov, V.;
Teterina, I.

Publication type:

Article

Gas Dynamics of a Recessed Nozzle in Its Displacement in the Radial Direction.

Published in:

Journal of Engineering Physics & Thermophysics, 2017, v. 90, n. 4, p. 932, doi. 10.1007/s10891-017-1640-8

By:

Volkov, K.;
Denisikhin, S.;
Emel'yanov, V.

Publication type:

Article

Thermodynamic substantiation of the existence of a phase transition point with a change in the structure of the solid-fuel mixture glycidyl azide Polymer/RDX.

Published in:

Journal of Engineering Physics & Thermophysics, 2012, v. 85, n. 5, p. 1058, doi. 10.1007/s10891-012-0747-1

By:

Futko, S.

Publication type:

Article

Sensitivity of combustion and ignition characteristics of the solid-fuel charge of the microelectromechanical system of a microthruster to macrokinetic and design parameters.

Published in:

Journal of Engineering Physics & Thermophysics, 2012, v. 85, n. 4, p. 874, doi. 10.1007/s10891-012-0726-6

By:

Futko, S.;
Ermolaeva, E.;
Dobrego, K.;
Bondarenko, V.;
Dolgii, L.

Publication type:

Article

Influence of temperature conditions in outer space on the macrokinetic characteristics of ignition and combustion of the solid-fuel charge of the microthruster of a microelectromechanical system.

Published in:

Journal of Engineering Physics & Thermophysics, 2012, v. 85, n. 2, p. 388, doi. 10.1007/s10891-012-0664-3

By:

Futko, S.;
Bondarenko, V.;
Dolgii, L.

Publication type:

Article

Macrokinetic calculation of the ignition of a solid-fuel charge of glycidyl azide polymer in the mini-engine of a microelectromechanical system.

Published in:

Journal of Engineering Physics & Thermophysics, 2011, v. 84, n. 6, p. 1304, doi. 10.1007/s10891-011-0598-1

By:

Fut'ko, S.;
Ermolaeva, E.;
Dobrego, K.;
Bondarenko, V.;
Dolgii, L.

Publication type:

Article

Simulation of the internal dynamics of solid-fuel rocket engines on the basis of the STAR-CD suite.

Published in:

Journal of Engineering Physics & Thermophysics, 2006, v. 79, n. 4, p. 678, doi. 10.1007/s10891-006-0153-7

By:

Volkov, K.;
Denisikhin, S.;
Emel’yanov, V.

Publication type:

Article

Design and Performance of Modular 3-D Printed Solid-Propellant Rocket Airframes.

Published in:

Aerospace (MDPI Publishing), 2017, v. 4, n. 2, p. 17, doi. 10.3390/aerospace4020017

By:

Hernandez, Rachel N.;
Singh, Harpreet;
Messimer, Sherri L.;
Patterson, Albert E.

Publication type:

Article

Design of the testing system for solid propellant rocket motor thrust measurements using mathematical modelling techniques.

Published in:

Journal of Measurements in Engineering, 2015, v. 3, n. 4, p. 123

By:

Fedaravičius, Algimantas;
Račkauskas, Saulius;
Survila, Arvydas;
Pataienė, Laima

Publication type:

Article

Burn-back Equations for High Volumetric Loading Single-grain Dual-thrust Rocket Propellant Configuration.

Published in:

Defence Science Journal, 2011, v. 61, n. 2, p. 165, doi. 10.14429/dsj.61.41

By:

Shekhar, Himanshu

Publication type:

Article

Failure Mode Avoidance of Solid Rocket Motor Pressure Monitoring Joint Seals.

Published in:

Journal of Failure Analysis & Prevention, 2017, v. 17, n. 6, p. 1191, doi. 10.1007/s11668-017-0356-6

By:

Murugesan, V.;
Sreejith, P.;
Anilkumar, A.;
Kishorenath, V.

Publication type:

Article

Flight Overloading Effect on the Working-Process Instability in the Combustion Chamber of a Solid-Fuel Rocket Engine.

Published in:

Doklady Physics, 2004, v. 49, n. 9, p. 527, doi. 10.1134/1.1810579

By:

Davydov, Yu. M.;
Davydova, I.M.;
Egorov, M. Yu.

Publication type:

Article

On the Ratio of Fréchet Random Variables.

Published in:

Quality & Quantity, 2006, v. 40, n. 5, p. 861, doi. 10.1007/s11135-005-5484-5

By:

Nadarajah, Saralees;
Kotz, Samuel

Publication type:

Article

Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions.

Published in:

International Journal of Aerospace Engineering, 2022, p. 1, doi. 10.1155/2022/4608619

By:

Sun, Lin;
Jia, Huiyin;
Zhang, Nan;
Zhao, Yu;
Bao, Futing

Publication type:

Article

Coupling of Level Set and Volume of Fluid Methods for Simulations of Transient Internal Flow Field in Solid Rocket Motors.

Published in:

International Journal of Aerospace Engineering, 2021, p. 1, doi. 10.1155/2021/2984992

By:

Zhang, Ze;
Gao, Feng;
Lv, Rui;
Gao, Yang

Publication type:

Article

Instantaneous Impact Point Guidance with Coast Arcs for Solid Rockets.

Published in:

International Journal of Aerospace Engineering, 2021, p. 1, doi. 10.1155/2021/5571877

By:

Jia, Shengwei;
Li, Fugui;
Tong, Mingbo

Publication type:

Article

Flow modeling in a porous cylinder with regressing walls using semi analytical approach.

Published in:

International Journal of Multiphysics, 2015, v. 9, n. 1, p. 75, doi. 10.1260/1750-9548.9.1.75

By:

Azimi, Mohammadreza;
Hedesh, Ali Montazeri;
Karimian, Saeed

Publication type:

Article

Electrospray Deposition of Energetic Polymer Nanocomposites with High Mass Particle Loadings: A Prelude to 3D Printing of Rocket Motors.

Published in:

Advanced Engineering Materials, 2015, v. 17, n. 1, p. 95, doi. 10.1002/adem.201400151

By:

Huang, Chuan;
Jian, Guoqiang;
DeLisio, Jeffery B.;
Wang, Haiyang;
Zachariah, Michael R.

Publication type:

Article

Analysis of efficiency of using hybrid propulsion for accelerating small-size rockets starting from the earth surface.

Published in:

Journal of Applied Mechanics & Technical Physics, 2010, v. 51, n. 6, p. 792, doi. 10.1007/s10808-010-0099-6

By:

Fomin, V.;
Zvegintsev, V.;
Mazhuls, I.;
Shumskii, V.

Publication type:

Article

一种改进型远程火箭弹发动机点火装置.

Published in:

Ordnance Industry Automation, 2022, v. 41, n. 9, p. 83, doi. 10.7690/bgzdh.2022.09.018

By:

杨青山;
赵成文;
刘波;
李泽亨;
王旭兵;
尚育生

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

Iran's Ballistic Missiles.

Published in:

Strategic Assessment: A Multidisciplinary Journal on National Security, 2009, v. 12, n. 2, p. 29

By:

Shapir, Yiftah S.

Publication type:

Article

Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner.

Published in:

International Journal of Aerospace Engineering, 2012, p. 1, doi. 10.1155/2012/673838

By:

Fanton, Luciano;
Paravan, Christian;
De Luca, Luigi T.

Publication type:

Article

Transient Burning Rate Model for Solid Rocket Motor Internal Ballistic Simulations.

Published in:

International Journal of Aerospace Engineering, 2008, p. 1, doi. 10.1155/2008/826070

By:

Greatrix, David R.

Publication type:

Article

Review of ultrasonic testing technology for bonding interfaces of solid rocket motors.

Published in:

Insight: Non-Destructive Testing & Condition Monitoring, 2021, v. 63, n. 11, p. 648, doi. 10.1784/insi.2021.63.11.648

By:

Ji, W. S.;
Zhou, Z. L.;
Zhang, H.;
Zheng, S.

Publication type:

Article

Mathematical modelling of the X-ray image of solid rocket motor for quantitative analysis.

Published in:

Insight: Non-Destructive Testing & Condition Monitoring, 2006, v. 48, n. 1, p. 21, doi. 10.1784/insi.2006.48.1.21

By:

Ravindran, V. R.;
Sreelekshmi, C.;
Pillai, V. P. Mahadevan

Publication type:

Article

Studies on the properties of EPDM-CSE blend containing HTPB for case-bonded solid rocket motor insulation.

Published in:

Polymers for Advanced Technologies, 2008, v. 19, n. 2, p. 144, doi. 10.1002/pat.988

By:

Sureshkumar, M. S.;
Bhuvaneswari, C. M.;
Kakade, S. D.;
Gupta, M.

Publication type:

Article

Solid propellant combustion in a high-velocity cross-flow of gases (review).

Published in:

Combustion, Explosion, & Shock Waves, 2016, v. 52, n. 5, p. 497, doi. 10.1134/S0010508216050014

By:

Arkhipov, V.;
Zarko, V.;
Zharova, I.;
Zhukov, A.;
Kozlov, E.;
Aksenenko, D.;
Kurbatov, A.

Publication type:

Article

Mechanism of the negative erosion effect.

Published in:

Combustion, Explosion, & Shock Waves, 2013, v. 49, n. 3, p. 273, doi. 10.1134/S0010508213030039

By:

Sabdenov, K.;
Erzada, Maira

Publication type:

Article

Method of the model equation in the theory of unsteady combustion of a solid propellant.

Published in:

Combustion, Explosion, & Shock Waves, 2012, v. 48, n. 1, p. 64, doi. 10.1134/S0010508212010091

By:

Rashkovskii, S.;
Milekhin, Yu.;
Klyuchnikov, A.;
Fedorychev, A.

Publication type:

Article

Coagulation of a liquid condensate of aluminum oxide in the combustion chamber of a solid rocket motor.

Published in:

Combustion, Explosion, & Shock Waves, 2011, v. 47, n. 1, p. 55, doi. 10.1134/S0010508211010072

By:

D'yachenko, N.;
D'yachenko, L.

Publication type:

Article

Analysis of the possibility of steady-state operation of a small-size solid-propellant thruster.

Published in:

Combustion, Explosion, & Shock Waves, 2009, v. 45, n. 5, p. 579, doi. 10.1007/s10573-009-0069-6

By:

Gusachenko, L. K.;
Rychkov, A. D.;
Kiskin, A. B.

Publication type:

Article