A flight test of the Aero jet Engineering Corporation's 7KS-6000 T-27 Jato rocket motor was conducted at the Langley Pilotless Aircraft Research Station at Wallops Island, Va, to determine the flight performance characteristics of the motor. The flight test imposed an absolute longitudinal acceleration of 9.8 g upon the rocket motor at 2.8 seconds after launching. The total impulse developed by the motor was 43,400 pound-seconds, and the thrusting time was 7.58 seconds. The maximum thrust was 7200 pounds and occurred at 4.8 seconds after launching. No thrust irregularities attributable to effects of the flight longitudinal acceleration were observed. Certain small thrust irregularities occurred in the flight test which appear to correspond to irregularities observed in static tests conducted elsewhere. A hypothesis regarding the origin of these small irregularities is presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Flight Test of the Aerojet 7KS-6000 T-27 Jato Rocket Motor


    Beteiligte:

    Erscheinungsdatum :

    1949-12-20


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Lightplane Jato seen in rocket design

    Engineering Index Backfile | 1947




    Bantam Family of Aerojet Rocketdyne Commercial Rocket Engines

    Levack, Daniel J. / Sack, William F. | AIAA | 2013


    Liquid-hydrogen rocket engine development at Aerojet, 1944 - 1950

    Osborn, G. H. / Gordon, R. / Coplen, H. L. et al. | NTRS | 1977