1–9 von 9 Ergebnissen
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    Simplified analysis of arcjet thrusters

    MARTINEZ-SANCHEZ, M. / SAKAMOTO, A. | AIAA | 1993

    Deflection of Multicellular Inflatable Tubes for Redundant Space Structures

    Hiraku Sakamoto / M. C. Natori / Yasuyuki Miyazaki | AIAA | 2002

    Deflection of multi-cellular inflatable tubes for redundant space structures

    Sakamoto, Hiraku / Natori, M. / Miyazaki, Yasuyuki | AIAA | 2001

    Magnetohydrodynamics Accelerator Performance with ...

    Anwari, M. / Sakamoto, N. / Hardianto, T. et al. | AIAA | 2005

    Comparative study of recessed and non-recessed swirl coaxial injectors

    Sasaki, M. / Sakamoto, H. / Takahashi, M. et al. | AIAA | 1997

    LOX/LH2 subscale swirl coaxial injector testing

    Tamura, H. / Sakamoto, H. / Takahashi, M. et al. | AIAA | 1997

    Numerical prediction of the flow characteristics in an arc wind tunnel

    MITSUDA, M. / KUROSAKA, T. / SAKAMOTO, Y. et al. | AIAA | 1992

    Mission scheduling expert system and its space station applications

    YOSHIOKA, T. / KATO, T. / WAKAKI, T. et al. | AIAA | 1987

    New concept of small satellite, HETE-2 and its sci...

    Matsuoka, M. / Kawai, N. / Yoshida, A. et al. | AIAA | 2005