Boron Particle Combustion in Solid Rocket Ramjets-Reference-Cited by-同舟云学术

Boron Particle Combustion in Solid Rocket Ramjets

Author:

Liu Daoping¹,Xia Zhixun²,Huang Liya³,Hu Jianxin⁴

Affiliation:

1. Ph.D. Candidate, Science and Technology, Scramjet Laboratory, National Univ. of Defense Technology, Changsha 410073, China.

2. Professor of Science and Technology, Scramjet Laboratory, National Univ. of Defense Technology, Changsha 410073, China (corresponding author).

3. Lecturer, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China.

4. Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

Reference19 articles.

2. Gany A. (2013). “Thermodynamic limitation on boron energy realization in ramjet propulsion.” 64th Int. Astronautical Congress Beijing China.

3. Boron particle ignition in secondary chamber of ducted rocket;Jianxin H.;Int. J. Aerosp. Eng,2012

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