Changes

== Propulsion ==

== Propulsion ==

The rocket will be powered by a M1230 from Cesaroni, which was chosen for several reasons. First, we determined that any M motor would be more powerful than necessary for the given weight and desired apogee <math>\sim</math> , however, the additon of sand weights would allow us to reach this altitude while staying subsonic. Second, this is a 75mm M motor which will allow us sufficient room on the exterior of a 98-75mm motor adapter to fill with sand.

The rocket will be powered by a M1230 from Cesaroni, which was chosen for several reasons. First, it allows us to attain our desired apogee ~ 10,000ft, and  second, this is a 75mm M motor which will allow us sufficient room on the exterior of a 98-75mm motor adapter to mount our static stability fins.

=== Motor Performance ===

=== Motor Performance ===

 

[[File:ThrustCurve M1230.png | right |650px]]

<span>m<span>0.3</span> m<span>0.7</span> </span>

 

[t]<span>0.3</span>

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=== Flight Characteristics ===

=== Flight Characteristics ===

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| 23.7 s

| 23.7 s

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== Structures ==

== Structures ==