Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Dept. of Space Transportation Eng., Inst. of Space and Astronautical Science
JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems
巻
JAXA-SP-05-010
ページ
111 - 114
発行年
2006-01-20
抄録(英)
RAMS (Residual Acceleration Measurement System) is sub-payload of M-V Rocket NO.6. This purpose is measurement of residual acceleration of B2 & B3 motor of M-V. This time, we get a long time data of the acceleration by means of RAMS & spacecraft's acceleration. This data is useful for analysis of Spacecraft separation, tracking of M-V. This paper describes the results of measurement of RAMS.