| Budget Amount *help |
¥4,290,000 (Direct Cost: ¥3,300,000、Indirect Cost: ¥990,000)
Fiscal Year 2011: ¥2,080,000 (Direct Cost: ¥1,600,000、Indirect Cost: ¥480,000)
Fiscal Year 2010: ¥780,000 (Direct Cost: ¥600,000、Indirect Cost: ¥180,000)
Fiscal Year 2009: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
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| Research Abstract |
The present space utilization expects that a combination of microsatellite of less than 100kg attains the operation efficiency and/or observation accuracy with comparison to the conventional large satellites, which can realized only by installation of propulsion system to such a microsatellite. For the purpose, this study aims to confirm the feasibility and development of integrated propulsion system for microsatellite of less than 50kg which is based on hydrogen peroxide and dimethyl ether.
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