Design of a Novel Hypersonic Inflatable Aerodynamic Decelerator for Mars Entry, Descent, and Landing
Skolnik, N.; Kamezawa, H.; Li, L.; Rossman, G.A.; Sforzo, B.; and Braun, R.D.; "Design of a Novel Hypersonic Inflatable Aerodynamic Decelerator for Mars Entry, Descent, and Landing," AIAA 2017-0469, 2017 AIAA Science and Technology Forum, Grapevine, TX, January 2017.