FLIGHT TEST OF THE AEROJET ~XS-6000 T-27 JATO ROCKET MOTOR

A flight test of the Aero jet Engineering Corporation's 75-6000 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 9.8g 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 secoads. 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 t m s t irregularities occurred in the flight test which appear to correspond to irregularities observed in static tests conducted elsewhere. A hy-pothesis regarding the origin of these small irregularities is presented