Numerical and Experimental Study of a 1-kW Hydrazine Engineering Design Model Arcjet Thruster-Reference-Cited by-同舟云学术

Numerical and Experimental Study of a 1-kW Hydrazine Engineering Design Model Arcjet Thruster

Published:2014-01 Issue:1 Volume:27 Page:16-25
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Tang Hai-Bin¹,Zhang Xin-Ai²,Liu Yu³,Wang Hai-Xing³,Wang Yi-Bai⁴

Affiliation:

1. Professor, School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China (corresponding author). E-mail address:

2. Ph.D. Candidate, School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China.

3. Professor, School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China.

4. Associate Professor, School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000213

Reference38 articles.

1. Arcjet thruster development

2. Bock D. Auweter-Kurtz M. and Kurtz H. L. (2005). “1 kW ammonia arcjet system development for a science mission to the moon.” Proc. 29th Int. Electric Propulsion Conf. IEPC-2005-075.

3. An advanced ammonia propellant feed system for the thermal arcjet TALOS;Bock D.;Proc., 43rd AIAA/ASME/ASEE Joint Propulsion Conf. and Exhibit,2007

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