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 self-level and transmit an unobstructed 360-degree image of the landing site.

Sub ScaleDesignFull Scale
Length [in]58.9120117
Stability
Margin [Cal.]		2.02.012.01
MotorAeroTech I300AeroTech L1390G
Rail Exit
Velocity [ft/s]		6863.663
Thrust / Weight Ratio5.945.94
CD0.530.490.49
Mw/Mbo1.081.10
Mpl [lb]66.34
Apogee [ft]142040003236
ParachuteFruity Chutes/CFC-36″Fruity Chutes/IFC-96″ Iris Ultra
Packing
Volume [in3]		27.3593.8545.2
BP Charge [g]Main: 1.5Drouge: 4
Main: 4		Drouge: 4
Main: 4

NASA Submittals

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