Works matching DE "SOLID propellant rockets"

Results: 69

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

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

The Use of Monte Carlo Simulation Methods to Calculate the Radiation of Jets of Combustion Products in View of Rotational Spectral Structure.

Published in:

High Temperature, 2003, v. 41, n. 5, p. 694, doi. 10.1023/A:1026157031016

By:

Surzhikov, S. T.

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

Development Results of Laser Ignition System for Solid Rocket Motor.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2021, v. 19, n. 5, p. 807, doi. 10.2322/tastj.19.807

By:

Keisuke MINAMI;
Yoshiki MATSUURA;
Koki KITAGAWA;
Satoshi ARAKAWA;
Naoki MORISHITA;
Toshiaki TAKEMAE;
Shota IWABUCHI;
Asato WADA;
Shinichiro TOKUDOME

Publication type:

Article

The Low-Cost Rocket with Low Melting Temperature Thermoplastic Propellant.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2019, v. 17, n. 3, p. 350, doi. 10.2322/tastj.17.350

By:

Hikaru ISOCHI;
Hikaru OTABE;
Tsutomu UEMATSU;
Nobuji KATO;
Keiichi HORI;
Yasuhiro MORITA;
Ryojiro AKIBA

Publication type:

Article

Development of a Near-field Intensity Measurement Capability for Static Rocket Firings.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 9

By:

GEE, Kent L.;
WHITING, Eric B.;
NEILSEN, Tracianne B.;
JAMES, Michael M.;
SALTON, Alexandria R.

Publication type:

Article

The Continuous Mixing Process of Composite Solid Propellant Slurry by an Artificial Muscle Actuator.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2016, v. 14, n. ists 30, p. 107

By:

Akihiro IWASAKI;
Kotaro MATSUMOTO;
Ryosuke BAN;
Shun YOSHIHAMA;
Taro NAKAMURA;
Hiroto HABU

Publication type:

Article

Experimental Study of Fragmentation of Hybrid Rocket Fuel.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 15

By:

Koki KITAGAWA;
Toru SHIMADA;
Yoshio NAKAYAMA;
Tomoharu MATSUMURA;
Kunihiko WAKABAYASHI;
Ryo TODA;
Takakazu MORITA

Publication type:

Article

Ignition Probability Improvement of a Laser-Ignition Micro Solid Rocket.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 37

By:

Tomoyuki HAYASHI;
Jun ASAKAWA;
Hiroyuki KOIZUMI;
Masakatsu NAKANO;
Kimiya KOMURASAKI

Publication type:

Article

First Launch in Months: Japan's Epsilon Launcher and Its Evolution.

Published in:

Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan, 2014, v. 12, n. ists 29, p. 21

By:

Yasuhiro MORITA;
Takayuki IMOTO;
Shinichiro TOKUDOME;
Hirohito OHTSUKA

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

GRAVITY MEASUREMENT METHOD OF SOLID ROCKET DRIVE BASED ON SWITCHED RELUCTANCE MOTOR SYSTEM.

Published in:

Thermal Science, 2021, v. 25, n. 6A, p. 4011, doi. 10.2298/TSCI2106011J

By:

Dongyi JIA;
Zhuo LI;
HAQI, Farooq;
YOUSUF, Mohammed

Publication type:

Article

EXPERIMENTAL STUDY ON COMPOSITE SOLID PROPELLANT MATERIAL BURNING RATE USING MATLAB ALGORITHM.

Published in:

Thermal Science, 2016, v. 20, p. S1119, doi. 10.2298/TSCI16S4119T

By:

THUNAIPRAGASAM, Selvakumaran;
NATARAJAN, Kadiresh

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

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

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

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

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

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

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

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

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

Design and Analysis of Solid Rocket Composite Motor Case Connector Using Finite Element Method.

Published in:

Polymers (20734360), 2022, v. 14, n. 13, p. 2596, doi. 10.3390/polym14132596

By:

Zhu, Lvtao;
Wang, Jiayi;
Shen, Wei;
Chen, Lifeng;
Zhu, Chengyan

Publication type:

Article

Extended Application and Experimental Verification of a New Erosive Burning Model Coupled Heat Transfer between Gas and Grain Based on a Star-Grain Solid Rocket Motor.

Published in:

Energies (19961073), 2022, v. 15, n. 4, p. 1564, doi. 10.3390/en15041564

By:

Sun, Lin;
Ma, Yanjie;
Bao, Futing;
Liu, Yang;
Hui, Weihua

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

A decision approach for multi-stage combined design of solid rocket.

Published in:

Enterprise Information Systems, 2021, v. 15, n. 8, p. 1179, doi. 10.1080/17517575.2020.1739341

By:

Meng, Yanli;
Wang, Li;
Wang, Lidong

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

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 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

Chemical processes in the HNF flame.

Published in:

Combustion, Explosion, & Shock Waves, 2006, v. 42, n. 5, p. 509, doi. 10.1007/s10573-006-0083-x

By:

Ermolin, N. E.;
Zarko, V. E.;
Keizers, H. H.

Publication type:

Article

Experimental Study of Thrust Performance of a Hybrid Rocket Motor with Various Methods of Oxidizer Injection.

Published in:

Combustion, Explosion, & Shock Waves, 2004, v. 40, n. 4, p. 386, doi. 10.1023/B:CESW.0000033560.34907.5e

By:

Potapkin, A. V.;
Lee, T.-S.

Publication type:

Article

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 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

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

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