The potential was examined of hydrogen-fueled supersonic vehicles designed for cruise at Mach 2.7 and at Mach 2.2. The aerodynamic, weight, and propulsion characteristics of a previously established design of a LH2 fueled, Mach 2.7 supersonic cruise vehicle (SCV) were critically reviewed and updated. The design of a Mach 2.2 SCV was established on a corresponding basis. These baseline designs were then studied to determine the potential of minimizing energy expenditure in performing their design mission, and to explore the effect of fuel price and noise restriction on their design and operating performance. The baseline designs of LH2 fueled aircraft were than compared with equivalent designs of jet A (conventional hydrocarbon) fueled SCV's. Use of liquid hydrogen for fuel for the subject aircraft provides significant advantages in performance, cost, noise, pollution, sonic boom, and energy utilization. (Author)


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    Title :

    Minimum Energy, Liquid Hydrogen Supersonic Cruise Vehicle Study


    Contributors:
    G. D. Brewer (author) / R. E. Morris (author)

    Publication date :

    1975


    Size :

    178 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Minimum energy, liquid hydrogen supersonic cruise vehicle study

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