Description of a new, medium-class Delta launch-vehicle configuration, the three-stage Model 2914. The first stage of this vehicle is composed of a liquid-propellant core which is thrust-augmented with up to nine strap-on solid-propellant motors. The second stage, recently uprated with a strap-down inertial guidance system, is now being modified to adapt the liquid-propellant descent engine from the Apollo Lunar Excursion Module. The third stage is a spin-stabilized solid-propellant motor. The Model 2914 is capable of injecting 2040 kg into low earth orbit, 705 kg into geosynchronous transfer orbit, or 455 kg into an escape trajectory.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    The Delta launch vehicle Model 2914 series


    Contributors:
    Gunn, C. R. (author)

    Conference:

    International Astronautical Congress ; 1973 ; Baku, Azerbaidzhan SSR


    Publication date :

    1973-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :