Payload and time-on-station performance of long endurance aircraft is shown for aircraft equipped with conventional and regenerative turboprop engines. Incorporation of laminar flow control on the airframe and addition of regeneration to helicopter engines is discussed; these two design considerations appreciably improve performance. Also, for helicopter missions in excess of approximately 2 hr duration, improvement in performance can be obtained by addition of regeneration process to the turboshaft engine cycle.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Application of Regenerative Engines to Projected Air Force Missions


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE World Congress & Exhibition ; 1964



    Publication date :

    1964-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Application of regenerative engines to projected air force missions

    Brock, J.E. / Gershon, I.J. | Engineering Index Backfile | 1964


    Regenerative water supply for long-duration missions

    Samsonov, N. M. / Bobe, L. S. / Novikov, V. M. et al. | British Library Conference Proceedings | 1998


    Projected NASA power requirements for space science and exploration missions

    Bennett, Gary L. / Pilcher, Carl B. / Smith, William L. | NTRS | 1992


    Regenerative System for Turboprop Engines

    Agrawal, Rishabh / Singh, Deepanshu / Subbarao, PMV | AIAA | 2017


    Projected NASA Power Requirements for Space Science and Exploration Missions

    Pilcher, Carl B. / Bennett, Gary L. / Smith, William L. | SAE Technical Papers | 1992