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Overview

Project Hermes is the team's entry to the 2018 IREC Unlimited Category. It is entirely SRAD. The design was conceived during summer of 2017. It is a single stage, 6in, minimum diameter rocket with a single separation point.

 Flight History:

Flight
Vehicle
Motor
Launch Site
Date
Result

Hermes Flight 1

Hermes 1OW-152-4G #3Friends of Amateur RocketryJuly 21, 2018Complete Success

 

Link to integration procedure: Hermes Integration Procedure

Link to Concept Design Review: Concept Design Review.pptx

Responsible Engineers Listed Here.

Mass Budget here.

June 2017 - Present
Leveraging existing technology for extreme performance
Liftoff Mass: ~156 lbs
Propellant Mass: ~68 lbs
Maximum Velocity: ~Mach 3
Maximum Apogee: ~ 80,000ft
Maximum Acceleration:

Leadership

President
VP
Treasurer
Social Chair
Pub. Chair
Charlie GAndrew RIsaac PMaddie JJoanna Z
StructuresPayloadRecoveryPropulsionAvionics
Matthew CMaddie GMaddie JSam AJosef B

Subsystems

Hermes Recovery System

The Hermes recovery system is a piston-actuated, single separation-dual deploy architecture.

Rumbler

Hermes Propulsion System (8-grain) is an eight-grain custom solid rocket motor that will provide propulsion for the vehicle.

Hermes Structures System

The Hermes Structures system.

Vehicles

Raziel Pathfinder

Raziel Pathfinder was an unflown Test Article from 2016-2017's Project Raziel. After undergoing extensive modifications, the pathfinder was uprated to flight hardware. The construction of this vehicle is primarily E-glass. Early manufacturing limitations limit the maximum length of any tube produced using the old methods to 24in, so the fin can is held together with a coupler. Some of the tubes are distinctly out of round due to a low-quality mandrel used for initial production runs. The nosecone is a modified COTS gelcoat covered 4:1 Ogieve nose cone.

Hermes I

Hermes I is the first build of a flight-ready Hermes rocket. Details to follow IAP 2018.

 

 

Deliverables

Project Hermes_Entry Form.xls

200_1st Progress Update.xls

 

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