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- W2205340983 abstract "An innovative Panel ExTension SATellite (PETSAT) and propulsion system for PETSAT, are presented in this paper. First, we outline what PETSAT is. Next, based on PETSAT ethos, design policy of the propulsion system is provided. According to the policy, we designed propulsion system and concretely estimated and assembled mono-propellant and bipropellant systems, and it indicated that monopropellant propulsion with 50-60 seconds of specific impulse and 1 N of thrust is probable. In the case of bi-propellant, 120-150 seconds of specific impulse is valid even based on the design policy. We conducted captive tests of mono-propellant and bi-propellant propulsions with a breadboard model of propulsion system for PETSAT, and obtained good operations and performances. Based on the test results, we designed and manufactured flight model propulsion system for PETSAT. We are planning to demonstrate it in SOHLA-2L project progressed by the Space Oriented Higashiosaka Leading Association (SOHLA). SOHLA-2L will be the first on-orbit demonstrator of PETSAT in 2008." @default.
- W2205340983 created "2016-06-24" @default.
- W2205340983 creator A5038150108 @default.
- W2205340983 date "2007-07-08" @default.
- W2205340983 modified "2023-10-18" @default.
- W2205340983 title "Demonstration of Propulsion System for Microsatellite Based on Hydrogen Peroxide in SOHLA-2 Project" @default.
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- W2205340983 doi "https://doi.org/10.2514/6.2007-5575" @default.
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