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→Launch Vehicle Summary: update
The purpose of the launch vehicle is to reach an apogee of approximately 11,800 ft and completely separate into two sections. The motor section will consist of one set of 4 stability fins and will fall to the ground using a reefing system. The payload section will deploy a reefing system and will contain actuating canards to stabilize the payload's decent.
The purpose of the launch vehicle is to reach an apogee of approximately 11,800 ft and completely separate into two sections. The motor section will consist of one set of 4 stability fins and will fall to the ground using a reefing system. The payload section will deploy a reefing system and will contain actuating canards to stabilize the payload's decent.
The forward airframe will be 40 in long and the aft airframe will be 45 in long, both with an inner diameter of 4 in and made of fiberglass. The total weight will be approximately 25.5 lbs loaded. We have selected to use the Intelli-Cone from Public Missiles and a CTI L395 motor with main deployment at 800 ft.
== Payload Summary ==
== Payload Summary ==