作者: Keir C. Gonyea , Robert D. Braun , Aaron H. Auslender
DOI: 10.2514/1.A33959
关键词: Descent (aeronautics) 、 Environmental science 、 Propulsion 、 Mars Exploration Program 、 Aerospace engineering 、 Breathing 、 Supersonic speed
摘要: Analysis was performed to assess the impact of atmospheric-breathing supersonic retropropulsion as a technology solution for Mars descent. Vehicle models were developed three architectures, emp...