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This script calculates the lifting force in Newtons and the lifting mass in Kg of a volume of hot air. You input the target air temperature of the canopy and it’s volume. The script currently presumes an ambient air temperature of 15 C with a standard air pressure value of 1.225Kg/M^3.
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682 Bytes |
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This script calculates templates for truncated conical transitions for rocket airframes. You input d1 and d2 as the end diameters matching the rocket airframe dimensions and you input the desired length. The function returns two radii, R1 and R2 and an angle, Theta, with which you can create a template.
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466 Bytes |
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