Lightweight power source for two 2' diameter propellors

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SUMMARY

The discussion focuses on finding a lightweight, high-output power source for a manned aircraft utilizing twin caged propellers with a diameter of 2 feet. Participants highlight the trade-offs between batteries and capacitors, noting that while capacitors offer higher power output, they lack sufficient energy capacity for sustained flight. The need for an optimal solution that balances weight and power efficiency is emphasized, particularly for VTOL applications.

PREREQUISITES
  • Understanding of VTOL (Vertical Take-Off and Landing) aircraft design
  • Knowledge of energy storage systems, specifically batteries and capacitors
  • Familiarity with power-to-weight ratios in aviation
  • Basic principles of propulsion and aerodynamics
NEXT STEPS
  • Research advanced battery technologies, such as lithium-sulfur batteries
  • Explore hybrid power systems combining batteries and capacitors
  • Investigate lightweight materials for aircraft construction
  • Learn about energy density and power density metrics in aviation applications
USEFUL FOR

Aerospace engineers, hobbyist aircraft designers, and anyone involved in the development of lightweight propulsion systems for manned aircraft.

Andrewlackey
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Hey everyone!

I am designing an experimental, manned aircraft that uses twin caged propellors for VTOL, and I'm looking for a lightweight, high-output power source to power them. Any ideas?
 
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