The work conducted by the ELORET Institute under this Cooperative Agreement includes the modeling of hypersonic propulsion systems and the evaluation of hypersonic vehicles in general and most recently hypersonic waverider vehicles. This work in hypersonics was applied to the design of a two-stage to orbit launch vehicle which was included in the NASA Access to Space Project. Additional research regarded the Oblique All-Wing (OAW) Project at NASA ARC and included detailed configuration studies of OAW transport aircraft. Finally, work on the modeling of subsonic and supersonic turbofan engines was conducted under this research program.


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    Title :

    Advanced Vehicle Concepts Systems and Design Analysis Studies


    Contributors:
    M. H. Waters (author) / L. C. Huynh (author)

    Publication date :

    1994


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Advanced vehicle concepts systems and design analysis studies

    Waters, Mark H. / Huynh, Loc C. | NTRS | 1994


    Advanced vehicle system concepts

    Hardy, K.S. / Langendoen, J.M. | Tema Archive | 1983


    Advanced launch vehicle concepts

    Bono, P. | Engineering Index Backfile | 1963


    Advanced Design Concepts for Onboard LNG Vehicle Tanks

    Bunger, U. / Owren, G. / International Gas Union et al. | British Library Conference Proceedings | 1995


    Advanced launch vehicle concepts

    Bono, P. | Engineering Index Backfile | 1963