Brown Space Engineers

Avionics Subgroup Fall 2024–Present

Joined Avionics subgroup in Sep 2024, continued role as RE for burn-wire mechanism. Through rapid prototyping (current measurements) with fishing line, determined feasibility of mechanism for camera arm and antenna deployment.

  • Elected as Avionics Lead Engineer in January 2025
  • Objectives:
    • Design PCBs for Electrical Power System (EPS), communications, power/data distribution, on-board computer, magnetorquer control, photodiode photocurrent amplification (for attitude determination and control systems algorithm), and more.
    • Train new members to begin contributing to projects
    • Work with integration REs to have prototyped and tested boards by EOY 2025.
  • Key requirements
    • Frequent and proactive communication with other subgroup leads to ensure alignment on tasks
    • Active recruiting to gain new members
    • Collaboration with engineering professors and BSE alumni in places where members are lacking experience
  • Project management approach: Weekly working group, leaders group, and frequent communication on Slack channels
  • Challenges encountered:
    • Lack of consistent member attendance
    • Knowledge gap for both members and leaders
    • Logistical and miscommunications leading to project standstills
  • Outcomes
    • Drafted PCBs for compute board
    • Breakout board for photodiode photocurrent amplification
    • Schematic planned for magnetorquer control board
    • UHF and EPS boards outsourced to OreSat, open-source CubeSat development group
    • Burn wire circuit designed and layout in progress
BSE Compute Board V1 for FlatSat, the EOY goal of all critical systems functional on a flat workbench.
Constant current circuit from Thurn et al. 2012, reference for nichrome burn wire deployment method

Structures Subgroup Fall 2022–Spring 2024

In Structures subgroup, aided in CAD design of CubeSat chassis and acted as responsible engineer for deployables.

  • Objective: Investigate potential designs for camera arm and antenna deployment
  • Key requirements
    • 3U CubeSat
    • Limited power, room on CubeSat
    • Reliability & electrically safe
  • Project management approach: Weekly working group and Slack channels
  • Challenges encountered: design difference from reference literature
  • Outcomes: Selected nichrome burn-wire design as outlined in Thurn et al. 2012