Unsteady chemical kinetics behavior of AP/HTPB propellant with micro-scale model
Author:
Affiliation:
1. School of Energy and Power Engineering, Nanjing University of Science and Technology, Nanjing Jiangsu, China
2. China Electronics Technology Group Corporation No.38 Research Institute, Hefei Anhui, China
Funder
Fundamental Research Funds for the Central Universities
Foundation Research Project of Jiangsu Province
Publisher
Informa UK Limited
Subject
General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry
Link
https://www.tandfonline.com/doi/pdf/10.1080/00102202.2018.1494594
Reference32 articles.
1. Burning Rate of Solid Propellant Ingredients, Part 1: Pressure and Initial Temperature Effects
2. Flash pyrolysis of hydroxyl-terminated polybutadiene (HTPB) I: Analysis and implications of the gaseous products
3. COMBUSTION OF SOLID PROPELLANT SANDWICHES: EFFECT OF BINDER OXYGENATION AND FINITE PECLET NUMBER
4. Burning Rate Characteristics of Ammonium Perchloarte-Based Composite Propellant Using Bimodal Ammonium Perchlorate
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