Retrorocket Soft Landing of Airdropped Cargo
Abstract:
A retrorocket soft landing system for airdropped cargo is described and mathematically analyzed. Solid propellant rockets and fixed height ground sensing, previously used in the experimental Parachute Retrorocket Airdrop System PRADS, are assumed for this system. Seventeen variables affecting the load impact velocity are defined and used to write the one-body equations of motion for the system. A computer is used to generate 500 constrained random values for each independent variable, to calculate the impact velocity for 500 cases by solving the equations of motion, and to statistically analyze the results. It is concluded that 95 of the soft landings can be expected to have impact velocities between 2.0 and 3.4 ms 6.1 and 10.3 fts.