Science Results of NOZOMI Mission
スポンサーリンク
概要
- 論文の詳細を見る
NOZOMI was the first Japanese mission to Mars. It was launched on 4 July, 1998 (JST) by M-V-3 launcher. The primary scientific objective of NOZOMI was to study the structure and dynamics of Martian upper atmosphere with emphasis on its interaction with the solar wind and 14 scientific instruments were carried on NOZOMI. Due to the malfunction of electronics parts, Mars orbit insertion was abandoned on 9 Dec. 2003 and NOZOMI mission was terminated. However some of the onboard instruments made observations both near the Earth and during cruise phase to Mars. This paper briefly describes the science results obtained by NOZOMI mission.
- 特定非営利活動法人 日本ロケット協会の論文
特定非営利活動法人 日本ロケット協会 | 論文
- Current Status of Rocket Developments in Universities -Development of a Small Rocket without Combustion Process
- Cost Comparison between HEO Satellites and 3G Wireless Mobile Phonos for Nationwide Ambulance Network
- The Avionics System Design Concepts for the Advanced Solid Rocket
- Autonomous Functions of NOZOMI Attitude and Orbit Control System and Mars Imaging Camera
- Precise Orbit Determination for ALOS and the Accuracy Verification by SLR