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RAMAC37 Activities at CARDC

  • Sen LiuEmail author
  • Zhiyong Bai
  • Hexiang Jian
Chapter
Part of the Shock Wave Science and Technology Reference Library book series (SHOCKWAVES, volume 10)

Abstract

The RAMAC, short for ram accelerator, is a relatively new concept of hypervelocity launcher. It was first proposed by Prof. A. Hertzberg of the University of Washington (UW) in 1980s [1]. The principle of a ram accelerator is similar to that of a ramjet/scramjet engine. The projectile, similar in shape to the center-body of a ramjet, is launched by an initial launcher such as a powder gun or gas gun, at a certain velocity and then enters a stationary tube filled with premixed gaseous propellant (typically combustible gas, oxygen and diluents).

Keywords

Mach Number Fill Pressure Average Acceleration Projectile Velocity Entrance Velocity 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Notes

Acknowledgements

The authors are grateful to our colleagues from the Hypervelocity Aerodynamics Institute of CARDC for their excellent work on RAMAC37. They are Prof. GAO Dongzhe, Mrs. PING Xinhong, Mr. BU Shaoqing, HUANG Qian, ZOU Qiongfen, YU Ziquan, LUO Jinyang, DU Hongjun, XIA Sheng, LI Yandong, ZHANG Weidong, YANG Chunying, HE Guishen, LIU Xiaolong, SHI Jianzhi, ZHANG Changgen and WANG Di. The authors would like to thank Prof. A. Hertzberg, Prof. A.P. Bruckner and Dr. C. Knowlen of University of Washington for their inspiring information on ram accelerator, and their help offered to Dr. LIU Sen when he studied at UW as a visiting scholar in the year of 2000.

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Copyright information

© Springer International Publishing Switzerland 2016

Authors and Affiliations

  1. 1.Hypervelocity Aerodynamics Institute (HAI)China Aerodynamics Research and Development Center (CARDC)MianyangPeople’s Republic of China

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