Several propulsion concepts lend themselves to application in tactical missiles; many of them can improve missile system performance by means of longer range, high speed, or both. Tactical missile propulsion systems generally fall into one of two categories: rockets that carry all their fuel and oxidizer and airbreathing engines that have to carry only their fuel since their oxidizer is obtained from the surrounding air. Tactical missiles were typically propelled by conventional solid propellant powered rockets or, occasionally, liquid propellant powered rockets. However, newly emerging requirements and needs are placing more emphasis on sustained high speed and longer ranges, as well as reduced cost and improved reliability and safety. In addition, there is more emphasis on launcher (aircraft or ground based) survivability. Survivability can be enhanced by longer ranges or reduced visibility. These needs can be implemented either singly or in combination by using selected propulsion systems. Pulse rockets, ramjets (both liquid fueled and solid fueled), turbojets, and air-turborockets (or turboramjets) possess the potential of long range and high speeds. An overview is provided for the various propulsion concepts considered applicable to tactical missiles and describes and discusses the merits of each.


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    Titel :

    Overview of Propulsion Concepts for Tactical Missiles


    Beteiligte:
    F. C. Zarlingo (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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    Sorensen, O.C. | Engineering Index Backfile | 1964


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    THOMAS, M. / CHRISTENSEN, K. | AIAA | 1994


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    Horton, M.P. | Tema Archiv | 1995