A solar thermal upper stage (STUS) is envisioned as a propulsive concept for the future. The STUS will be used for low Earth orbit (LEO) to geostationary-Earth orbit (GEO) transfer and for planetary exploration missions. The STUS offers significant performance gains over conventional chemical propulsion systems. These performance gains translate into a more economical, more efficient method of placing useful payloads in space and maximizing the benefits derived from space activity. This paper will discuss the economical advantages of an STUS compared to conventional chemical propulsion systems, the potential market for an STUS, and the recent activity in the development of an STUS. The results of this assessment combined with the performance gains, will provide a strong justification for the development of an STUS.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Solar Thermal Upper Stage: Economic Advantage and Development Status


    Contributors:
    A. M. Adams (author)

    Publication date :

    1995


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    Development status of Ariane-5 upper stage

    Holsten, H. / Association Aeronautique et Astronautique de France / Royal Aeronautical Society et al. | British Library Conference Proceedings | 1994


    Development status of Ariane-5 upper stage

    Holsten, H. | British Library Online Contents | 1994