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Effects of four isocyanates and four plasticizers on the thermomechanical and tensile properties of hydroxyl‐terminated polybutadiene elastomers and the effect of solid particle filling

Journal of applied polymer science, 2021-05, Vol.138 (18), p.n/a

2021

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The Connection Between the Parameters of WLF Equation and of Arrhenius Equation

Propellants, explosives, pyrotechnics, 2019-06, Vol.44 (6), p.696-705

Bohn, Manfred A.

2019

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On the functionalization and characterization of hydroxyl‐terminated polybutadiene with octyl‐1‐azide and the evaluation of polyurethane elastomers based on such modified HTPB

Journal of applied polymer science, 2021-03, Vol.138 (10), p.n/a

2021

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Simulation of Heat Flow Curves of NC‐Based Propellants – Part 1: Determination of Reaction Enthalpies and Other Characteristics of the Reactions of NC and Stabilizer DPA Using Quantum Mechanical Methods

Propellants, explosives, pyrotechnics, 2021-08, Vol.46 (8), p.1188-1203

2021

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Problems and faulty uses with the Prout–Tompkins description of autocatalytic reactions and the solutions

Journal of thermal analysis and calorimetry, 2014-05, Vol.116 (2), p.1061-1072

Bohn, Manfred A.

2014

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Simulation of Heat Flow Curves of NC‐Based Propellants – Part 2: Application to DPA Stabilized Propellants

Propellants, explosives, pyrotechnics, 2021-08, Vol.46 (8), p.1204-1215

2021

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Characterization of Aging Behavior of Butacene® Based Composite Propellants by Loss Factor Curves

Propellants, explosives, pyrotechnics, 2017-07, Vol.42 (7), p.712-723

2017

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Aging of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements

Propellants, explosives, pyrotechnics, 2013-04, Vol.38 (2), p.190-198

2013

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Insensitive high explosives: VI. experimental determination of the chemical compatibility of nitroguanidine with seven high explosives

Propellants, explosives, pyrotechnics, 2024-02, Vol.49 (2), p.n/a

2024

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Characterization of Gun Propellants by Long‐Term Mass Loss Measurements

Propellants, explosives, pyrotechnics, 2017-07, Vol.42 (7), p.706-711

2017

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Activation energies for the decomposition of nitrate ester groups at the anhydroglucopyranose ring positions C2, C3 and C6 of nitrocellulose using the nitration of a dye as probe

Polymer degradation and stability, 2014-04, Vol.102, p.49-58

2014

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Characterization of ADN/GAP-Based and ADN/Desmophen®-Based Propellant Formulations and Comparison with AP Analogues

Propellants, explosives, pyrotechnics, 2014-04, Vol.39 (2), p.192-204

2014

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Prediction of In-Service Time Period of Three Differently Stabilized Single Base Propellants

Propellants, explosives, pyrotechnics, 2009-06, Vol.34 (3), p.252-266

Bohn, Manfred A.

2009

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Solid‐Liquid Adhesion Energies of Composite Propellant Components Determined by Solution Calorimetry

Propellants, explosives, pyrotechnics, 2017-07, Vol.42 (7), p.728-735

2017

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Novel theoretical and computer-assisted modeling of isothermal and non-isothermal depolymerization kinetics

Polymer testing, 2015-07, Vol.44, p.1-7

2015

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Aging of ADN Rocket Propellant Formulations with Desmophen®-Based Elastomer Binder

Propellants, explosives, pyrotechnics, 2014-08, Vol.39 (4), p.526-537

2014

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Aging of Standard and Insensitive RDX Crystals Investigated by Means of X‐Ray Diffraction

Propellants, explosives, pyrotechnics, 2017-07, Vol.42 (7), p.724-727

2017

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Microstructure of the HMX-Based PBX KS32 after Mechanical Loading

Propellants, explosives, pyrotechnics, 2015-12, Vol.40 (6), p.880-885

2015

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Decomposition Pathways of Ammonium Dinitramide (ADN) and its HNO 3 ‐Clusters Elucidated by DFT‐Calculations

Propellants, explosives, pyrotechnics, 2021-02, Vol.46 (2), p.233-244

2021

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Thermal ageing of rocket propellant formulations containing ε-HNIW (ε-CL20) investigated by heat generation rate and mass loss

Thermochimica acta, 2003-05, Vol.401 (1), p.27-41

Bohn, Manfred A.

2003

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Kinetic Description of Mass Loss Data for the Assessment of Stability, Compatibility and Aging of Energetic Components and Formulations Exemplified with ε-CL20

Propellants, explosives, pyrotechnics, 2002-06, Vol.27 (3), p.125-135

Bohn, Manfred A.

2002

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DFT and G2MP2 Calculations of the N-N Bond Dissociation Enthalpies and Enthalpies of Formation of Hydrazine, Monomethylhydrazine and Symmetrical and Unsymmetrical Dimethylhydrazine

Zeitschrift für Naturforschung. B, A journal of chemical sciences, 2004-02, Vol.59 (2), p.148-152

2004

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Aging of ADN Rocket Propellant Formulations with Desmophen registered -Based Elastomer Binder

Propellants, explosives, pyrotechnics, 2014-08, Vol.39 (4), p.526-537

2014

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Characterization of ADN/GAP-Based and ADN/Desmophen registered -Based Propellant Formulations and Comparison with AP Analogues

Propellants, explosives, pyrotechnics, 2014-04, Vol.39 (2), p.192-204

2014

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AMMONIUM DINITRAMIDE/GLYCIDYL AZIDE POLYMER (ADN/GAP) COMPOSITE PROPELLANTS WITH AND WITHOUT METALLIC FUELS

International journal of energetic materials and chemical propulsion, 2017, Vol.16 (1), p.61-79

2017

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Effects of four isocyanates and four plasticizers on the thermomechanical and tensile properties of hydroxyl‐terminated polybutadiene elastomers and the effect of solid particle filling

The Connection Between the Parameters of WLF Equation and of Arrhenius Equation

On the functionalization and characterization of hydroxyl‐terminated polybutadiene with octyl‐1‐azide and the evaluation of polyurethane elastomers based on such modified HTPB

Simulation of Heat Flow Curves of NC‐Based Propellants – Part 1: Determination of Reaction Enthalpies and Other Characteristics of the Reactions of NC and Stabilizer DPA Using Quantum Mechanical Methods

Problems and faulty uses with the Prout–Tompkins description of autocatalytic reactions and the solutions

Simulation of Heat Flow Curves of NC‐Based Propellants – Part 2: Application to DPA Stabilized Propellants

Characterization of Aging Behavior of Butacene® Based Composite Propellants by Loss Factor Curves

Aging of HTPB/Al/AP Rocket Propellant Formulations Investigated by DMA Measurements

Insensitive high explosives: VI. experimental determination of the chemical compatibility of nitroguanidine with seven high explosives

Characterization of Gun Propellants by Long‐Term Mass Loss Measurements

Activation energies for the decomposition of nitrate ester groups at the anhydroglucopyranose ring positions C2, C3 and C6 of nitrocellulose using the nitration of a dye as probe

Characterization of ADN/GAP-Based and ADN/Desmophen®-Based Propellant Formulations and Comparison with AP Analogues

Prediction of In-Service Time Period of Three Differently Stabilized Single Base Propellants

Solid‐Liquid Adhesion Energies of Composite Propellant Components Determined by Solution Calorimetry

Novel theoretical and computer-assisted modeling of isothermal and non-isothermal depolymerization kinetics

Aging of ADN Rocket Propellant Formulations with Desmophen®-Based Elastomer Binder

Aging of Standard and Insensitive RDX Crystals Investigated by Means of X‐Ray Diffraction

Microstructure of the HMX-Based PBX KS32 after Mechanical Loading

Decomposition Pathways of Ammonium Dinitramide (ADN) and its HNO 3 ‐Clusters Elucidated by DFT‐Calculations

Thermal ageing of rocket propellant formulations containing ε-HNIW (ε-CL20) investigated by heat generation rate and mass loss

Kinetic Description of Mass Loss Data for the Assessment of Stability, Compatibility and Aging of Energetic Components and Formulations Exemplified with ε-CL20

DFT and G2MP2 Calculations of the N-N Bond Dissociation Enthalpies and Enthalpies of Formation of Hydrazine, Monomethylhydrazine and Symmetrical and Unsymmetrical Dimethylhydrazine

Aging of ADN Rocket Propellant Formulations with Desmophen registered -Based Elastomer Binder

Characterization of ADN/GAP-Based and ADN/Desmophen registered -Based Propellant Formulations and Comparison with AP Analogues

AMMONIUM DINITRAMIDE/GLYCIDYL AZIDE POLYMER (ADN/GAP) COMPOSITE PROPELLANTS WITH AND WITHOUT METALLIC FUELS

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