Accession Number:

ADA517534

Title:

Conceptual Design Tool for Fuel-Cell Powered Micro Air Vehicles

Descriptive Note:

Master's Thesis

Corporate Author:

AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH GRADUATE SCHOOL OF ENGINEERING AND MANAGEMENT

Personal Author(s):

Report Date:

2010-03-01

Pagination or Media Count:

232.0

Abstract:

A conceptual design tool was built to explore power requirements of a hybrid-power system for Micro Air Vehicles MAVs comparable in size to the Coopers Hawk. An inviscid aerodynamic code, Athena Vortex Lattice AVL, and a motor-propeller analysis code, QPROP, provide overall lift, drag, and thrust data for power-required calculation as functions of many variables to include mass, platform geometry, altitude, velocity, and mission duration. Phoenix Technologies Model Center was used to integrate multi-disciplinary components that employ specific power and specific energy of two power sources to determine power system mass required for a designated mission. The tool simulated a mission for the fixed wing Generic Micro Aerial Vehicle GenMAV, and relative sizing between a high specific power source and a high specific energy source was investigated. Current small fuel cell technology provides inadequate specific power. It was found that a MAV-sized fuel cell-battery hybrid-power system would not perform better than a pure battery or battery-battery power system. A feasible fuel cell capability requirement of at least 325 Wkg matched with at least 921 W-hrkg was identified as a fuel cell - Li-Po solution for a defined 30 min mission resulting in reduced power system mass compared to using only Li-Po batteries.

Subject Categories:

  • VSTOL
  • Pilotless Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE