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  • Research on ADN Green Propulsion Technology for Fast-Responding Satellite Applications

    Paper number

    IAC-13,C4,6,1,x18048

    Author

    Mr. Jialong JI, China Academy of Space Technology (CAST), China

    Coauthor

    Mr. Shuisheng Sun, China

    Coauthor

    Mr. Jun Chen, China Academy of Space Technology (CAST), China

    Coauthor

    Mr. Fenglin Ding, China Academy of Space Technology (CAST), China

    Coauthor

    Mr. Ming He, China Academy of Space Technology (CAST), China

    Year

    2013

    Abstract
    The novel technology of satellite propulsion with green propellant has been widely drawing our attention and widely studied since it was put forward. The advantage of liquid Ammonium Dinitramide(ADN) based propellant for fast-responding satellites, compared with the common propellant used for satellites at present, is presented in this paper. According to the character of green propellant, the scheme of satellite propulsion system with liquid-state ADN as monopropellant is advanced, and the preliminary modularization design is carried out. Also, we have the green propulsion system design with ADN as propellant, which is of the same as the working principle of common small satellite platform's propulsion system, and we have some calculations for fast-responding satellites. The calculation shows that because of the high density-specific impulsion and consistency of ADN based propellant, the green propulsion system can be used in fast-responding satellites.
    Abstract document

    IAC-13,C4,6,1,x18048.brief.pdf

    Manuscript document

    IAC-13,C4,6,1,x18048.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.