Performance Analysis of a Thermoelectric Combined Power Cycle

Author:

Xie Kan1,Yi Xiaolong1ORCID,Chen Jiang1,Yan Dongfeng1

Affiliation:

1. Beijing Institute of Technology, Beijing 100081, China

Funder

Advanced Space Propulsion Laboratory of Beijing Institute of Control Engineering and Beijing Engineering Research Center of Efficient and Green Aerospace Propulsion Technology

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference26 articles.

1. Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane

2. LiuP. “Investigation on Performance and Influence Factors of Rocket Ejector Mode of RBCC,” Ph.D. Dissertation, College of Astronautics, Northwestern Polytechnical Univ., China, 2001 (In Chinese).

3. Progress in Astronautics and Aeronautics;Siebenhaar A.,2000

4. Combined Rocket and Airbreathing Propulsion Systems for Space-Launch Applications

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