Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Ignition Characteristics of a Laser Ablation Igniter in a GO~x/GH~2 Thruster


    Contributors:
    Mori, K. (author) / Kusaka, K. (author) / Fujita, K. (author) / Niino, M. (author) / Nakajima, S. (author) / Arakawa, Y. (author)

    Conference:

    International symposium; 23rd, Space technology and science; Proceedings of the twenty-third international symposium on space technology and science



    Publication date :

    2002-01-01


    Size :

    6 pages


    Remarks:

    Conference held in 2 volumes



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Aerospace Laser Ignition/Ablation Variable High Precision Thruster

    Campbell, Jonathan W. / Edwards, David L. / Campbell, Jason J. | NTRS | 2015


    Ignition powder and igniter comprising same

    IWASAKI KOJU | European Patent Office | 2024

    Free access

    Modular Ignition System Based on Resonance Igniter

    M. Niwa / A. Santana / K. Kessaev | AIAA | 2001


    B/Ti multilayer reactive igniter for micro solid rocket array thruster

    Tanaka, S. / Kondo, K. / Habu, H. et al. | Tema Archive | 2007


    Igniter, igniter device, and igniter manufacturing method

    SABAMEK JOACHIM / KOMORI SHOGO / FUJII KOHEI | European Patent Office | 2024

    Free access