Experimental Study on Electrical Ignition Characteristics of Ammonium Dinitramide based Propellant under Different Environmental Pressures

Author:

Li Lei12,Li GuoXiu12,Li HongMeng12,Yao ZhaoPu3

Affiliation:

1. School of Mechanical, Electronic and Control EngineeringBeijing Jiaotong University No. 3 Shangyuancun, Haidian District Beijing 100044 P. R. China

2. Key Laboratory of Vehicle Advanced ManufacturingMeasuring and Control Technology (Beijing Jiaotong University) Ministry of Education No. 3 Shangyuancun, Haidian District Beijing 100044 P. R. China

3. Aerospace Propulsion Product Research CenterBeijing Institute of Control Engineering No. 16 South 3rd Street, Zhongguancun, Haidian District Beijing 100190 P. R. China

Funder

Fundamental Research Funds for the Central Universities

National Natural Science Foundation of China

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Reference47 articles.

1. M. Negri. Replacement of Hydrazine: Overview and First Results of the H2020 Project Rheform.6thEuropean Conference for Aeronautics & Space Sciendes. Krakow Poland 29 May- 03 July 2015.

2. Future chemical propellants for space, defense, and commercial applications;Perut C.;Int. J. Energ. Mater. Chem. Propul.,2007

3. Nanocrystallisation of Ammonium DiNitramide (ADN) by Spray Flash Evaporation (SFE).;Edouard B. J.;Propellants Explos. Pyrotech.,2018

4. An Overview on the Synthetic Routes and Properties of Ammonium Dinitramide (ADN) and other Dinitramide Salts

5. Combustion of Propellants with Ammonium Dinitramide

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