Downloads & Free Reading Options - Results

A concept for aerial delivery of supplies by dropping modules vertically through bottom doors in an aircraft was investigated. Preliminary analysis was conducted to determine the effect on the aircraft structural weight, strength, and aerodynamic performance. A preliminary design of the mechanical cargo handling system was completed. The dynamic effect of dropping cargo on the stability and control characteristics of the aircraft was investigated. The system was evaluated in comparison to a conventional aerial delivery system for typical missions performed by a forward-area transport. The concept was shown to be advantageous for performing resupply missions when operating in the vertical flight mode. It is concluded that the concept has potential application to V/STOL or rotary-wing aircraft.