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Hermes III: November 24, 2019 Shake TestHermes III Avionics Tower Force TestingHermes 3 Reaction Wheel ProposalHermes III Payload Bulkhead

 

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Notes (2/19/23):

  • Look into commercial vibrational testers - Claire

  • Screw terminal loose – was this the cause of avionics turning on? → Talk to avionics

  • Talk to Avionics about required components for upper and lower avionics towers - Emily

  • Calculate space above AV tower needed to store parachute - Julianne

    • Look at and dimension Phoenix booster mission package tube

    • 4 components: parachute area for 1st stage, AV bay, parachute area for 2nd, motor

  • Start CADing slider AV tower

  • Researc extra forces on AV tower from parachutes, potential buckling

Timeline:

  • 1st meeting points:

    • How many avionics towers, what does the deployment look like (probably won't be decided) *Assigned

    • Approximate dimensioning, looking into what the mass would be for these systems assuming Phoenix Avionics systems weights and lengths *Assigned

      • Sustainer:

        • Weight:

        • Length:

      • Booster

        • Weight:

        • Length:

    • *Need an estimate of board size from avionics

  • Issue of the bay turning on in transit:

    • Did the vibration of the system cause the screw to move? If so, we may need better screw switches. This one was highly reviewed by rocketry forum: https://www.csrocketry.com/electronics/missleworks.html

    • *I need someone to come up with the test and give me commercial vibrational testers

  • Incorporating a window for easy access
  • *Calculations for bay sizing
  • packing volume of the lines and prevent potential line entanglement issues.
  • Mathinline
    bodyL=\frac{4V}{\pi D^{2}}
     
  • 𝐿=4𝑉/𝜋𝐷^2
  • LaTeX Math Block
    anchorV = \frac{w_{parachute}}{\rho_{packing}}
    V = \frac{w_{parachute}}{\rho_{packing}}


  • 𝑉=𝑃𝑎𝑟𝑎𝑐ℎ𝑢𝑡𝑒 𝑤𝑒𝑖𝑔ℎ𝑡/𝑃𝑎𝑐𝑘𝑖𝑛𝑔 𝑑𝑒𝑛𝑠𝑖𝑡𝑦

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