Experimental Investigation of μN-class Laser Ablation Thruster

• SUMIDA Sota

  Department of Aeronautics and Astronautics, Tokai University

• HORISAWA Hideyuki

  Department of Aeronautics and Astronautics, Tokai University

• FUNAKI Ikkoh

  Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

Abstract

The micro-Newton thrust measurement was conducted for a low intensity continuous wave laser thruster for aluminum foil propellant target. To evaluate the thrust characteristics, a torsion-balance thrust stand capable for the measurement of the thrust level down to micro-Newton range was developed. In the case of the aluminum foil target, the maximum thrust level was 6 μN when the laser power was 20 W. It was also found that the laser intensity, or laser power per unit area, irradiated on the target was significantly important on the control of the thrust even under the low-intensity level.

Journal

• TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN

  TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN 7 (ists26), Pb_159-Pb_162, 2009

  THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Keywords

• Electric Propulsion
• Laser Propulsion
• Laser Ablation

Details

• CRID: 1390282680191346176
• NII Article ID: 130000259574
• DOI: 10.2322/tstj.7.pb_159
• ISSN: 13473840
• Web Site: https://www.jstage.jst.go.jp/article/tstj/7/ists26/7_ists26_Pb_159/_pdf
• Text Lang: en
• Data Source:
  • JaLC
  • Crossref
  • CiNii Articles
  • KAKEN
• Abstract License Flag: Disallowed