Mission Objective

The launch vehicle will deliver a payload to an apogee altitude between 3,500 and 5,500 feet above ground level (AGL). The payload must then retrieve a minimum of 10 mL sample from one of five designated sites around the launch pad and transport it at least 10 feet.

Sub ScaleDesignFull Scale
Length [in]68.25135136
Stability
Margin [Cal.]		2.02.42.26
MotorAeroTech I284AeroTech L2200G
Rail Exit
Velocity [ft/s]		677368
Thrust / Weight Ratio26.78.878.06
CD1.00.590.59
Mw/Mbo1.171.111.10
Mpl [lb]98.65
Apogee [ft]175245004454
ParachuteFruity Chutes/CFC-30″Fruity Chutes/IFC-144″ Iris Ultra
Packing
Volume [in3]		27.3466.5466.5
BP Charge [g]Drouge: 3.5
Main: 5.5		Drouge: 3.5
Main: 5.5

NASA Submittals

Prelim. Design Review
Critical Design Review
Flight Readiness Review
Post Launch Review