The Diagnostics Testbed Facility (DTF) at NASA's John C. Stennis Space Center in Mississippi was designed to provide a testbed for the development of rocket engine exhaust plume diagnostics instrumentation. A 1200-lb thrust liquid oxygen/gaseous hydrogen thruster is used as the plume source for experimentation and instrument development. Theoretical comparative studies have been performed with aerothermodynamic codes to ensure that the DTF thruster (DTFT) has been optimized to produce a plume with pressure and temperature conditions as much like the plume of the Space Shuttle Main Engine as possible. Operation of the DTFT is controlled by an icon-driven software program using a series of soft switches. Data acquisition is performed using the same software program. A number of plume diagnostics experiments have utilized the unique capabilities of the DTF.


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    Titel :

    A subscale facility for liquid rocket propulsion diagnostics at Stennis Space Center


    Beteiligte:
    Raines, N. G. (Autor:in) / Bircher, F. E. (Autor:in) / Chenevert, D. J. (Autor:in)

    Erscheinungsdatum :

    01.06.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    A Subscale Facility for Liquid Rocket Propulsion Diagnostics at Stennis Space Center

    Chenevert, D. J. / Bircher, F. E. / Raines, N. G. | SAE Technical Papers | 1991



    Overview of Rocket Propulsion Testing at NASA Stennis Space Center

    Rahman, S. / Gilbrech, R. / Lightfoot, R. et al. | NTRS | 1999