Leadership
| | | | |
---|
Andrew A | Colin P/Andrew K | Dayna E | Martina S | Charlie G |
Structures | Payload | Recovery | Propulsion | Avionics |
---|
Amy V | James R/Martina S | Maddie J | Zach B | Andrew R |
Vehicles
Raziel Pathfinder
Raziel Pathfinder was designed to be test flown in early December 2016. It was completed in November 2016. The vehicle used an E Glass composite structure with a West Systems epoxy. The fin can was in two components, joined by a coupler. The vehicle was designed to be single-sep, dual deploy, with a large quadcopter containing lander on top.
Raziel 1
Raziel 1 was the first flight vehicle in Project Raziel. It was switched to a dual separation architecture and uses a sabot to deploy the payload. The airframe was constructed from S glass and System 3000 epoxy from Fiberglast. The vehicle flew in Maryland at LDRS 36.
Flights:
Design Reviews:
PDF |
---|
name | Project Raziel- PDR 2016-2017.pdf |
---|
|
PDF |
---|
name | Project Raziel PDR _VALLEDOR.pdf |
---|
|
PDF |
---|
name | MIT Rocket Team CDR Presentation Slides.pdf |
---|
|
Experimental Sounding Rocket Association Deliverables (Spaceport America Cup 2017)