Perform a temporo-spatial integration of the internal ballistics of a hybrid rocket engine. Use equation (16-1) for
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Question:
Perform a temporo-spatial integration of the internal ballistics of a hybrid rocket engine. Use equation (16-1) for the regression rate. If necessary, you may avoid the singularity near x = 0 by using equation (16.2) in this region.
Parameters
L = 5 m
d = .3 m
D = 1 m
a = .036
A* = .025 m2
rhop = 920 kg/m3
m dot ox = 20 kg/s
The fuel is HTPB, and the oxidizer is O2.
Use these curve fits for reference.
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