Bimodal space reactor systems provide both thermal propulsion for the spacecraft orbital transfer and electrical power to the spacecraft bus once it is on station. These systems have the potential to increase both the available payload in high energy orbits and the available power to that payload. These increased mass and power capabilities can be used to either reduce mission cost by permitting the use of smaller launch vehicles or to provide increased mission performance from the current launch vehicle. A major barrier to the deployment of these bimodal systems has been the cost associated with their development. This paper describes a bimodal reactor system with performance potential to permit more than 70 % of the instrumented payload of the Titan IV/Centaur to be launched from the Atlas IIAS. The development cost is minimized by basing the design on existing component technologies.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    A bimodal power and propulsion system based on cermet fuel and heat pipe energy transport


    Additional title:

    Ein bimodales Kraft- und Antriebssystem basierend auf Cermet Treibstoff- und Wärmerohrenergietransport


    Contributors:


    Publication date :

    1995


    Size :

    6 Seiten, 8 Bilder, 10 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Bimodal power and propulsion system based on cermet fuel and heat pipe energy transport

    G. F. Polansky / N. A. Gunther / R. F. Rochow et al. | NTIS | 1995


    Bimodal spacecraft bus based on a cermet fueled heat pipe reactor

    G. F. Polansky / R. F. Rochow / N. G. Gunther et al. | NTIS | 1995


    A bimodal spacecraft bus based on a cermet fueled heat pipe reactor

    Polansky, Gary / Rochow, Richard / Gunther, Norman et al. | AIAA | 1995