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PROPENSITY is a prospective project for flight on a new, large hybrid
motor. If constructed, it will also test some new construction
techniques, such as using a strong internal core with an outer shell of
Quik-Tube. Initial flights would be on a cluster of solid motors, and later flights would be on
a central hybrid with
a very long tank and an outboard cluster of solid motors. In this
configuration, the vehicle should be capable of altitudes up to 90,000
feet. PROPENSITY would also test a new "payload bay
door" parachute ejection system. We have settled on a final
design and are currently running CFD and stress calculations.
CAD Models
Chris found time to create a couple of CAD models of PROPENSITY on the
computer, using Catia. He is currently running simulations on the various
sections of the airframe to insure strength parameters are met while maintaining
a reasonable propellant mass fraction and overall vehicle weight.
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| Model of the interior of the
avionics bay |
Nose cone structure model --
base view |
Nose cone structure model --
side view |
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| Nose cone model
with 0.093" Fe mesh applied |
Fin can model |
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