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The 3-d drawings for the sustainer and its cross-section view can be found below.

                                                     

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                                                   Figure 1: Sustainer.

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Here, the thrust curve for the sustainer can be found.

                                        Figure 3: Sustainer thrust curve. 

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The divergence and convergence half angles are 15.0 and 60.0 degrees, respectively. A close-up 3-d drawing of the nozzle can be found below.

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                                                                 Figure 4: Cross-section view of the sustainer nozzle.

 

Grains

The propellant used in both motors of the rocket is the Cherry Limeade. 

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