NASA NTRS · 20170003394
Mission and Design Sensitivities for Human Mars Landers Using Hypersonic Inflatable Aerodynamic Decelerators
Abstract
This paper explores the impact of human Mars mission architecture decisions on the design and performance of a lander using the HIAD entry system: (a) Earth departure options, (b) Mars arrival options, (c) Entry Descent and Landing options.
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Polsgrove, Tara, Thomas, Herbert D., Dwyer Cianciolo, Alicia, Collins, Tim, Samareh, Jamshid. 2017-03-07. Mission and Design Sensitivities for Human Mars Landers Using Hypersonic Inflatable Aerodynamic Decelerators. https://ntrs.nasa.gov/citations/20170003394
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