Accession Number : ADA291666
Title : The Performance of Cargo Airdrop Systems Using G-12E Parachutes: Statistical Determination of Minimum Altitude.
Descriptive Note : Final rept. Mar 93-Nov 94,
Corporate Author : ARMY NATICK RESEARCH DEVELOPMENT AND ENGINEERING CENTER MA
Personal Author(s) : Kunz, Steven E.
PDF Url : ADA291666
Report Date : FEB 1995
Pagination or Media Count : 42
Abstract : In order to reduce the exposure of aircraft to hostile fire, the U.S. Air Force is interested in dropping cargo from the lowest possible altitude above ground level. Using trajectory data from previous airdrop system testing, this report statistically determines the minimum altitude above ground level (AOL) from which airdrop systems (comprising clusters of two to three G-12E parachutes) may safely deliver cargoes up to 5000 pounds. The methods used to compute variables of interest, such as system tension and system orientation, are presented. To support this statistical analysis, intervals were defined based upon clearly discernible events. This led to a reexamination of so-called functional phases, used by the airdrop community. Some phases were found unsuitable for statistical purposes. To resolve this problem, process intervals were defined based upon clearly discernible process states or events. Based upon the limited data available, it was found that G-12E airdrop systems can safely deliver cargoes of up to 5000 pounds when released from aircraft at an altitude of approximately 300 feet AGL. (AN)
Descriptors : *CARGO PARACHUTES, TEST AND EVALUATION, GROUND LEVEL, STATISTICAL DATA, TENSION, CARGO, DROP TESTS, WIND VELOCITY, AIR DROP OPERATIONS, STATISTICAL ANALYSIS, DRAG, TRAJECTORIES, DETERMINATION, AERIAL DELIVERY, LOW ALTITUDE.
Subject Categories : Gliders and Parachutes
Distribution Statement : APPROVED FOR PUBLIC RELEASE