Results 91 to 100 of about 467 (183)

Comminution of energetic materials in viscous binder components with high solid loadings

, 2018
S.120.1-120.10Wet comminution enables the production of very fine energetic particles direct in binder components. Besides the processing of energetic materials, the general high viscosities of binder materials are challenging.
Dresel, Alexander, Gerber, Peter, Heintz, Thomas, Roßmann, Christian   +3 more
core   +1 more source

Experimental Studies on Advanced Sheet Explosive Formulations Based on 2,4,6,8,10,12-Hexanitro-2,4,6,8,10,12-hexaazaisowurtzitane (CL-20) and Hydroxyl Terminated Polybutadiene (HTPB), and Comparison with a RDX-based System

, 2016
The present investigation reports the use of 2,4,6,8,10,12-hexanitro2,4,6,8,10,12-hexaazaisowurtzitane (CL-20) in sheet explosive formulations. In this study, hydroxyl terminated polybutadiene (HTPB) based sheet explosives were prepared incorporating the
Singh, M. K., Jangid, S. K., Sinha, R. K., Talawar, M. B., Nath, T.   +4 more
core  

Polyurethane Based Inhibition for High Flame Temperature Nitramine Based Composite Modified Double Base propellant

, 2013
The findings for polypropylene glycol (PPG) and hydroxyl-terminated polybutadiene (HTPB)-based inhibition systems are reported. These findings established that the inhibition system comprising HTPB-IPDI-IDP binder and Sb/sub 2/O/sub 3/-C black filler
Khangaonkar, D. G., Asthana, S. N., Kadam, U. B., Kakade, S. D., Divekar, P. K., Vaidya, M. V.   +5 more
core   +2 more sources

Degradation and stabilisation of diisocyanate cured polybutadiene [PDF]

Hydroxyl terminated polybutadiene (HTPB) has been used as a rocket propellant binder which is required to be stored for at least twenty years. It is found that the excellent stress-strain characteristics of this propellant can be totally lost, during ...
Wang, Ting
core  

Stabilisation of isocyanate cross linked polybutadiene binder [PDF]

Isocyanate cross-linked hydroxy terminated polybutadiene is used as a binder for solid rocket propellant. Rocket motors containing this propellant require a storage life of at least 20 years.
Scott, Simon M.
core  

Effect of Curing Parameter on the Mechanical Properties and Bond Strength at Propellant-Liner Interfaces in Rocket Motors

Chemical Engineering Transactions
This study investigates the effect of curing parameters (Rt) on the mechanical properties and bond strength of propellants and liners in rocket motors compared to the design values.
Thirapat Kitinirunkul, Paisarn Boonyarat, Khumchoo Wasan, Apinan Namkanisorn   +3 more
doaj  

Development of nitrocellulose based binder for ammonium perchlorate/aluminium solid propellant

, 2013
In the manufacturing of solid propellants, a binder is used to bind a mixture of oxidizer and fuel particles uniformly. In this study, nitrocellulose was developed as a binder for ammonium perchlorate/aluminum solid propellant. Since nitrocellulose is in
Hafifi Abdullah, Mohd. Aliff
core  

Dynamic Mechanical Properties of HTPB - IPDI Binders of Four PBX with Different HMX Contents and Energetic Particles Augmented Binder

683732Energetically augmented or, in other words, energetic particle enhanced inert binder using hydroxyl-terminated polybutadiene (HTPB) prepolymer has attained some scientific notice in recent years [2-8]. The particles incorporated into the binder are
Gerber, Peter, Heintz, Thomas, Bohn, Manfred   +2 more
core   +1 more source

Development of composite solid propellent using dicyclopentadien binder

, 2010
Through the history of composite solid propellant binders new chemicals are introduced as binders to improve upon the previous generation. Sometimes this is done to improve upon the flaws or shortcomings of a previous binder.
Bluestone, Stephen Ray
core  

Improving Mechanical Properties of Carboxyl-Terminated Polybutadiene (CTPB) Binder System Using a Cure Accelerator. [PDF]

Molecules
Qu X, Hu P, Ma X, Liu Y, Yang H, Zhang W, Chen Y.   +6 more
europepmc   +1 more source