An overview of the research on the 20 tons H-2 Orbiting Plane (HOPE) is presented focusing on technical problems which greatly influences to the body weight. The purpose and missions of HOPE program, fundamental conditions, flight profile, approximate configuration and major dimensions, major performances, and concept of development are described.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Hope No Kenkyuu (Research on Hope)


    Contributors:
    T. Itou (author) / J. Kouchiyama (author) / Y. Takizawa (author) / H. Aoki (author) / A. Eguchi (author)

    Publication date :

    1992


    Size :

    4 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Shourai No Uchuuki Shisutemu No Kenkyuu (Research on Advanced Spacecraft)

    T. Iwata / T. Etou / R. Imai et al. | NTIS | 1992


    Research of H-2 Orbiting Plane (HOPE). 1. HOPE: System Concept

    T. Akimoto / T. Ito / H. Miyaba | NTIS | 1987


    Research of H-2 Orbiting Plane (HOPE). 3. HOPE: Guidance and Control System

    Y. Takizawa / S. Tanaka / T. Izumi et al. | NTIS | 1987