Forward Attached Inflatable Decelerators, more commonly known as inflatable aeroshells, provide an effective, cost efficient means of decelerating spacecrafts by using atmospheric drag for aerocapture or planetary entry instead of conventional liquid propulsion deceleration systems. Entry into planetary atmospheres results in significant heating and aerodynamic pressures which stress aeroshell systems to their useful limits. Incorporation of lightweight inflatable decelerator surfaces with increased surface-area footprints provides the opportunity to reduce heat flux and induced temperatures, while increasing the payload mass fraction. Furthermore, inflatable aeroshell decelerators provide the needed deceleration at considerably higher altitudes and Mach numbers when compared with conventional rigid aeroshell entry systems. Inflatable aeroshells also provide for stowage in a compact space, with subsequent deployment of a large-area, lightweight heatshield to survive entry heating. Use of a deployable heatshield decelerator not only enables an increase in the spacecraft payload mass fraction and but may also eliminate the need for a spacecraft backshell and cruise stage. This document is the viewgraph slides for the paper's presentation.
Aerocapture Inflatable Decelerator (AID)
19th AIAA Aerodynamic Decelerator Systems Technology Conference ; 2007 ; Williamsburg, VA, United States
2007-05-23
Conference paper
No indication
English
Aerocapture Inflatable Decelerator for Planetary Entry
NTRS | 2007
|Aerocapture Inflatable Decelerator (AID) for Planetary Entry
British Library Conference Proceedings | 2007
|NTIS | 1981
|NTIS | 1978
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