The development of a new family of launch vehicles by Lockheed Martin to support the current trend toward smaller, rapidly developed, cheaper spacecraft programs is described. An overview of the Lockheed Martin Launch Vehicle (LMLV) family of launch vehicles is provided, with specific discussion of the LMLV propulsion, avionics, structures, payload fairing options, and payload adapter and separation system options. LMLV's use of Thiokol's Star motors as injection stages is presented for mission requirements other than low Earth orbit. Typical launch environments at the spacecraft interface are identified, and the LMLV Program's special attention to reducing launch operations costs is presented through a discussion of LMLV's "stack-and-shoot" parallel-processing methodology; providing minimum interaction between the LMLV and spacecraft launch processing timelines. An overview of the standard LMLV launch services is presented, with discussion of the launch services flow, payload processing, and launch vehicle processing. Finally, the results of the first LMLV1 launch in August of 1995 are summarized, along with the current LMLV contract manifest.


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    Titel :

    The Lockheed Martin launch vehicle (LMLV) solution for small payloads


    Beteiligte:
    McCurry, J.B. (Autor:in) / Carter, W.P. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.01.1997


    Format / Umfang :

    1109537 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    The Lockheed Martin Launch Vehicle (LMLV): Solutions for Small Payloads

    Carter, W. P. / McCurry, J. B. / IEEE; Aerospace and Electronics Systems Society | British Library Conference Proceedings | 1997


    Lockheed Martin launch vehicle application to small planetary missions

    McCurry, J. B. / International Academy of Astronautics | British Library Conference Proceedings | 1996