Skip to content
Descubridor Institucional UMAR
Inicio
Búsqueda avanzada
Explorar
Inicio
Búsqueda avanzada
Explorar
Login
Language
English
Deutsch
Español
Français
Italiano
All Fields
Title
Author
Subject
Call Number
ISBN/ISSN
Tag
Find
Advanced
Indentation Method for Solid Rocket Motor Grain Material Mechanical Properties Testing
Indentation Method for Solid Rocket Motor Grain Material Mechanical Properties Testing
Fuente:
Wiley Open Access
Saved in:
Bibliographic Details
Main Authors:
Zijian Fan
,
Peng Yu
,
Kunlin Zhou
,
Zhenhang Ling
Format:
Artículo Open Access
Published:
Wiley
2025
Subjects:
Propellants, Explosives, Pyrotechnics
Online Access:
Acceder al recurso
Tags:
Add Tag
No Tags, Be the first to tag this record!
Cite this
Text this
Email this
Print
Export Record
Export to RefWorks
Export to EndNoteWeb
Export to EndNote
Save to List
Permanent link
Holdings
Description
Comments
Similar Items
Staff View
Internet
https://onlinelibrary.wiley.com/doi/10.1002/prep.70073
Similar Items
Shear Mechanical Properties Prediction Method and Simulation Calculation Model of Aging NEPE Propellant Adhesive Interface
by: Kunlin Zhou, et al.
Published: (2025)
Properties of Heterogeneous Solid Rocket Propellants Based on Poly(glycidyl azide) and Octogen
by: Katarzyna Cieślak, et al.
Published: (2026)
Formulation of Hexamine‐based Fuels for Hybrid Rockets
by: Niklas Wingborg
Published: (2024)
Pore Characteristics of NEPE Solid Propellant under Pressure Cure
by: Huihui Zhang, et al.
Published: (2026)
Experimental Study on the Effective Service Range of Hydroxyl‐terminated Polybutadiene Propellant Based on Indentation Theory
by: Xiaohong Gui, et al.
Published: (2025)