Results 211 to 220 of about 956,080 (280)

Effective Performance Modifications for a Composite Rocket Propellant via Coagglomerates of Cyclic Nitramines. [PDF]

ACS Omega
Patil VB, Lewczuk R, Sazeček F, Paziewska P, Stojan P, Bělina P, Zeman S.   +6 more
europepmc   +1 more source

Synthesis and UV-Curing Modification of the High cis-1,4-Hydroxyl-Terminated Polybutadiene Binder Suitable for Ultra-Low Temperature Applications. [PDF]

Polymers (Basel)
Lyu H, Wang L, Li Y, Yu G, Liu S, Sun D, Liang Y, Huo P, Zhang D, Ning Z, Kong X.   +10 more
europepmc   +1 more source

Advances in PBT Binder and Its Application in Propellants. [PDF]

Polymers (Basel)
Zhang N, Gao X, Luo Y, Zhang W, Xin Y, Zhang K, Xue C, Zhang H, Wei J, Wang H.   +9 more
europepmc   +1 more source

Experimental Study on the Evolution of Mechanical Properties and Their Mechanisms in a HTPB Propellant Under Fatigue Loading. [PDF]

Polymers (Basel)
Feng F, Chen X, Xu J, Zeng Y, Huang W, Dong J.   +5 more
europepmc   +1 more source

Deep-Neural-Networks-Based Data-Driven Methods for Characterizing the Mechanical Behavior of Hydroxyl-Terminated Polyether Propellants. [PDF]

Polymers (Basel)
Han R, Fu X, Qu B, Shi, Liu Y.
europepmc   +1 more source

Solid propellants: AP/HTPB composite propellants

Arabian Journal of Chemistry, 2019
AbstractIn this article we mainly discuss about AP/HTPB composite solid propellants. Classification, components, properties, burning rate and ignition behavior of propellants are mentioned here. Combustion of AP monopropellant, HTPB and AP/HTPB is discussed in detail.
Pragnesh N Dave, Shalini Chaturvedi
exaly   +2 more sources

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Detonability of Solid Composite Propellants

ARS Journal, 1961
The thin film pla t inum resistance thermometer (heat flux gage) has been successfully applied to measurement of heat fluxes from initiators for solid propellants. Hea t fluxes measured were as high as 1000 Btu/ft-sec from hot, particleladen reaction products of pyrotechnic igniters.
Andersen, W. H., Chaiken, R. F.
openaire   +2 more sources

Composite propellant combustion

AIAA Journal, 1970
Temperature measurements in gaseous reaction zone near surface of burning composite solid propellant, using modified line reversal ...
R. L. DERR, J. R. OSBORN
openaire   +1 more source

Prediction of the Critical Diameter of Composite Propellants

AIAA Journal, 1972
A theoretical model which predicts the critical diameter of composite propellants is presented. A previously published detonation model is corrected and refined by use of a new model which considers both single grain size AP and dual grain size AP configuration s, for both porous and nonporous propellants.
P. SALZMAN, T. DUNCAN
openaire   +1 more source

Nano-composites for rocket solid propellants

Composites Science and Technology, 2005
Aim of this work is the study of different components (binder and aluminum powders) of solid propellants used for rocket propulsion to improve ballistic performance. New propellant formulations have been tested and characterised. Combustion residues were collected by a proprietary method and analyzed both from the morphological and chemical point of ...
MEDA, LUISA MARINA, G. Marra, GALFETTI, LUCIANO, DE LUCA, LUIGI, F. Severini, S. Inchingalo   +5 more
openaire   +2 more sources