Sustainer and Its Cross-Section View
The 3-d drawings for the sustainer and its cross-section view can be found below.
Figure 1: Sustainer.
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Figure 2: Cross-section view of the sustainer.
Thrust Curve
Here, the thrust curve for the sustainer can be found.
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Figure 3: Sustainer thrust curve.
Motor Specifications and the Nozzle
This is an M1329 motor, with a total impulse of 5.8 kNs.
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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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Simulator Files
For reference, the motor simulation file can be found here: 5.8KNs_M1300_24in.ric
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