Atmospheric effects on Martian aerocapture

Abstract

A preliminary study of the effects of the atmosphere on Martian aerocapture has been completed at NASA-Johnson. Nominal cases were defined and several types of density dispersions utilized to show the effect of L/D ratio on aerocapture performance. Both open and closed loop three-degree-of-freedom simulations were developed. The open loop work demonstrated the reduction of the aerocapture corridor in the presence of density biases and shears. Closed loop runs were studied in the presence of shear-biases where the aerocapture trajectory was divided into three regions or phases. Each phase independently had a nominal density or a dispersed + 100 percent density. Two phase combinations were found to cause aerocapture failures with the three L/Ds considered: 0.3, 0.7, 1.0. There is a significant improvement in aerocapture performance as the L/D is increased from 0.3 to 0.7, but a much smaller increase in performance as the L/D is increased from 0.7 to 1.0. Based on current knowledge of the Martian atmosphere, a minimum L/D of 0.7 is recommended for early Mars missions.