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 Scale||Design||Full Scale|
|Motor||AeroTech I284||AeroTech L2200G|
|Thrust / Weight Ratio||26.7||8.87||8.06|
|Parachute||Fruity Chutes/CFC-30″||Fruity Chutes/IFC-144″ Iris Ultra|
|BP Charge [g]||Drouge: 3.5Main: 5.5||Drouge: 3.5Main: 5.5|