Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)), Sagamihara, Kanagawa Japan
抄録（英）
We have been studying the generalized propulsion system based on green mono/bi-propellant since 2008. While, the last achievements prove feasibility of the propulsion system and conducted captive test with a breadboard model (BBM), no ignition was confirmed there. Accordingly, we modified the ejector in thruster and measured droplet diameter of liquid propellant in combustion chamber, and improved performance of propellant atomization.
内容記述
形態: カラー図版あり
形態: CD-ROM1枚
内容記述（英）
Physical characteristics: Original contains color illustrations
Note: One CD-ROM
低毒性推進剤による二液式推進系の研究開発
