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We need to know the magnitude and location of the center of mass of all the rocket components. Once measured, these values must be added to the OpenRocket model.
Items in bold must be physically measured.
nosecone tip
0.2655 lbm, 38.423 in upstream of the nosecone interface (via SW)
OR model (Mass is overridden to zero, since the nosecone uses the integrated mass/CoM.)
nosecone shell
measurement
OR model (uses total mass/CoM of the shell-tip-rod assembly)
recovery system
measurement
OR model
18" module
measurement
OR model
24" module
measurement
OR model
fin can
measurement
OR model
spider
0.08 lbm (36 g), 0.39 in (10 mm) downstream of the male ring's interface (via SW)
OR model
cradle mount
0.3012 lbm, 0.4193 in upstream of the female ring, 0.2607 upstream of the male ring (via SW) Having it inside the next module upstream is a huge style no-no. Fortunately, we don't care about that for L-13.
OR model ()
cradle frame
measurement
OR model
cradle spacers
0.0898 lbm, 0.1625 in downstream of the male interface, 0.6425 in upstream of the female interface
OR model
These are probably already pretty accurate in the OR database:
engine casing
engine core
thrust flange ("motor mount", "pizza", etc.)
0.1771 lbm, 0.1800 in downstream of the female interface
OR model
camera module
measurement
OR model
umbilical module
measurement
OR model
telemetrum
measurement
OR model
RCS (any CoM estimate is vapor for now...)
measurement
OR model
The text was updated successfully, but these errors were encountered:
Rather than put everything here, I put my measurements in this file. (See the file for more info.)
E: the values have been added to the OR model. The modules were lighter than expected, the nosecone was heavier, and the fin can was basically dead-on. So, the stability margin caliber at Mach 0.3 decreased by 0.03 (trivial).
Hey @jejor, you should go measure the things. You'll need to get a recovery person to get the parachutes out for you... someone like @hmarie2 or @calvin-young.
We need to know the magnitude and location of the center of mass of all the rocket components. Once measured, these values must be added to the OpenRocket model.
Items in bold must be physically measured.
Having it inside the next module upstream is a huge style no-no. Fortunately, we don't care about that for L-13.
The text was updated successfully, but these errors were encountered: