Results 81 to 90 of about 467 (183)
Ceiling Temperature Influence on The Synthesis of MT-4 and Aging Behavior of Polyurethane Polymer
The stability of the bonding agent in the polymeric binder system has a significant impact on the long-term aging performance of composite solid rocket propellants (CSRPs).
Ali abdelall
doaj +1 more source
Mechanical properties of HTPB propellants: Recent advances and underlying mechanisms
Hydroxyl-terminated polybutadiene (HTPB)-based composite solid propellants (CSPs) are widely used in solid rocket motors due to their excellent mechanical properties and low cost.
Wasiullah Qazi +3 more
doaj +1 more source
Ionizing Radiation Sensitivity of Hydroxyl Terminated Polybutadiene Solid Propellant
The effects of ionizing radiation on hydroxyl-terminated polybutadiene (HTPB) solid propellant are investigated to assess its sensitivity to electron radiation. Investigation into the radiation sensitivity of HTPB propellant is needed to assess potential
Lopez, Juan C
core
Synthesis of propellant grade HHTPB by hydrogenation of HTPB using Pd-activated charcoal as catalyst
To derive more performance from the conventional composite propellant based on hydroxyl-terminated polybutadiene (HTPB) and ammonium perchlorate (AP), it is envisaged to hydrogenate HTPB, which increases the H/C (hydrogen to carbon ratio) of the base ...
Ch. Devi Vara Prasad +3 more
doaj +1 more source
Theoretical Investigation of the Bond Dissociation of Hydroxyl Terminated Polybutadiene Binder and Effect on Mechanical Properties [PDF]
Wen-Ming Wu +3 more
openaire +1 more source
Glycidyl Azide-Butadiene Block Copolymers: Synthesis from the Homopolymers and a Chain Extender
Glycidyl azide polymer (GAP) is an energetic alternative to hydroxyl-terminated polybutadiene (HTPB), but has poorer mechanical properties. Since HTPB-GAP mechanical blends are markedly biphasic, the use of block copolymers may be the solution to join ...
Cappello M. +3 more
core +2 more sources
5367Glycidyl azide polymer (GAP) is a promising energetic binder for solid propellants, but it suffers from poor mechanical properties compared to hydroxyl-terminated polybutadiene (HTPB).
Gettwert, Volker, Keicher, Thomas
core +1 more source
S.212-228Composite rocket propellants (CRP) contain oxidizer particles and fuel particles in an elastomeric binder matrix: The oxidizing agent is mostly ammonium perchlorate (AP) and the elastomer is hydroxyl terminated polybutadiene (HTPB) based ...
Bohn, Manfred A., Nardai, Michael M.
core
The regulation of the burning rate pressure exponent for the ammonium perchlorate/hydroxyl-terminated polybutadiene/aluminum (AP/HTPB/Al) composite propellants under high pressures is a crucial step for its application in high-pressure solid rocket ...
Jinchao Han, Songqi Hu, Linlin Liu
doaj +1 more source
The effect of replacing hexahydro-1,3,5-trinitro-1,3,5-triazine (RDX) by octahydro-1,3,5,7-tetranitro-1,3,5,7-tetrazocine (HMX) in HTPB-binder on the performance, sensitivity, thermal, and mechanical properties of the sheet explosive formulation has been
Krothapalli Prabhakara Subrahmania Murthy +9 more
core +2 more sources

