• Created by Unknown User (astrocrg@mit.edu), last modified by Unknown User (reilleya@mit.edu) on Sep 16, 2018 13:59

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Overview

 

On July 21, 2018 at Friends of Amateur Rocketry, Project Hermes launched a development vehicle to validate the Single Separation, Dual Deployment architecture and student researched propulsion. 

 

 

Flight Data Files

Pyxida: No File - Flash Error

Raven 3: 2.FIPa

TeleMetrum: 2018-07-21-serial-5102-flight-0002.eeprom

CAD

 

Video

Pictures

Hermes_up.JPG

RecoveryGroupPhoto.jpg

BehindtheLaunchButton.jpg

 

Simulator Files

hermes.CDX1

6in_35kNs_BATES_rev3.eng

 

Specifications

  • Launch mass: 121 lbs
  • Burnout mass: 86 lbs
  • Propulsion: OW-152-4G #3
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