1. A Self-Consistent Tension Shell Structure for Application to Aerobraking Vehicle and Its Aerodynamic Characteristics;Abe,1988
2. Examination of radio frequency blackout for an inflatable vehicle during atmospheric reentry;Takahashi;J. Spacecr. Rockets,2014
3. Supersonic inflatable aerodynamic decelerators for use on future robotic missions to Mars;Clark;J. Spacecr. Rockets,2009
4. Hypersonic Inflatable Aerodynamic Decelerator (HIAD) Technology Development Overview;Hughes,2011
5. M. Gräßilin, U. Schöttle, Flight Performance Evaluation of the Reentry Mission IRDT-1, in: Papers Presented at the 52nd International Astronautical Congress, IAF Paper 01-V305, Toulouse, France, October 1–5 2001.