This paper presents a measurement system for assessing the thrust produced by advanced aerospace propulsion nozzles. The system is able to evaluate the transverse components of thrust in the case of vectorized nozzles using three precision balances positioned at the base of the test rig. The balances are arranged in a 120-degree configuration to accurately reconstruct the thrust vector. Cold flow experiments using air as the working fluid are carried out for a linear aerospike nozzle in differential throttling configurations. A calibration of the thrust measurement system has been carried out.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Vectorized Thrust Measurement for Aerospace Propulsion Nozzles


    Beteiligte:


    Erscheinungsdatum :

    18.06.2025


    Format / Umfang :

    2786805 byte





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Maximum Thrust Nozzles

    WILLIAM E . CONWAY AND AARS CELMINS | AIAA | 1972



    Thrust coefficients of low-thrust nozzles

    Brinich, P. F. / Jack, J. R. / Spisz, E. W. | NTRS | 1965


    Thrust coefficients of low-thrust nozzles

    Spisz, Ernie W. / Brinich, Paul F. / Jack, John R. | TIBKAT | 1965