Interior ballistics calculations for nozzleless solid propellant rocket motors

Author:

COATS D.1,DANG L.1,NICKERSON G.1

Affiliation:

1. Software and Engineering Associates, Inc., Santa Ana, CA

Publisher

American Institute of Aeronautics and Astronautics

Reference25 articles.

1. to calculate the pressure and mass flow. The performance of the motor( delivered specific impulse, Isp ) i s then calculated by a

2. The two key parameters required of the igniter-ignition model for predictive purposes are the ignition delay time and the peak pressure. To date, the simple model used i n the NPP appears to predict the peak pressure well, but under predicts the ignition delay time significantly. Figures . 2-10 show the ignition sequence for head end, middle, and aft end igniters, respective 1y. The head end pressure trace, velocity prof i1es, and pressure profiles are displayed i n a comparative manner so that the salient features can be secn. The formation of right- and left-running waves i s readily seen as i s the development of a shock wave near the exit of the motor. Head end and middle of the grain igniters posz no problems i n running the computer model. However, the strong shock which forms when the pressure pulse from an aft end igniter i s reflected from the head end closure leads to computational difficulties. The flame speed used in the computations shown i n Figures 4, 7, and 10 was unrealistically high i n order to smooth out the steep fronted pulse from the igniter. Despite the overall poor prediction of the ignition delay, the peak pressure reached after ignition was predicted to within 1%for the DUE0 notor as shown i n Figure 17. Grain Geflection

3. The next set of Figures, 11 - 16, show the effect of grain deformation on the internal ballistics of a nozzleless soli d rocket motors. The calculations shown i n these figures do not include erosive burning or an igniter model (the grain was assumed to be instaneously ignited). Theonly difference i n the calculations are the presence of the grain deformation effects. The condition temperature for these cases was taken to be -65' i n order t o accentuate the grain deflection due to cooldown. The effects of the grain deformation are observed t o be most pronounced during the volume filling transient when visco-elastic effects are most important. The

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