The performance requirements of advanced technology-incorporating, next-generation heavy lift launch vehicles (HLLVs) for LEO missions are discussed, and the configurational features facilitated by those technologies are evaluated. These 1990s 'cargo' vehicles will capitalize on advanced avionics, software and automation, novel hot structure and thermal insulation materials, and more powerful liquid-fuel rockets employing either hydrogen or hydrocarbons. The configurations considered include a winged booster. The use of Space Shuttle components is a major cost-minimization strategy in many of these HLLV design efforts.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Advanced heavy lift launch vehicles


    Beteiligte:

    Kongress:

    Aerospace century XXI: Space flight technologies ; 1986 ; Boulder, CO, United States


    Erscheinungsdatum :

    01.01.1987


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Shuttle Evolved Heavy Lift Launch Vehicles

    Sauvageau, D. / Lounge, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003


    Shuttle Evolved Heavy Lift Launch Vehicles

    Lounge, John / Sauvageau, Donald | AIAA | 2003


    Heavy Lift Launch Vehicles with Existing Propulsion Systems

    Donahue, B. / Brady, L. / Farkas, M. et al. | British Library Conference Proceedings | 2010