The Adaptive Deployable Entry and Placement Technology (ADEPT) is being considered as an entry, descent and landing (EDL) system to enable Human Mars class missions. ADEPT is a mechanically deployable decelerator that makes use of a 3 d woven carbon fabric as both heat shield and primary structure. The Human Mars Mission design study is focused, in part, on assessing the viability of ADEPT and identifying technical challenges, operational constraints, and critical risk mitigation activities. To date, the study has found that, while the ADEPT concept has some design challenges, the scalability of the ADEPT system is viable and mass efficient for landing large masses at Mars. One issue found is as the size of the decelerator increases the convective heatflux decreases, along with the monatomic oxygen levels, moving the carbon surface-planetary atmospheric gas system into the kinetic oxidation regime. The current approach utilizes equilibrium thermochemistry to predict the mass loss due to oxidation which is overly conservative and results in a requirement for many more ablative layers than will truly be needed. The thicker the woven TPS structure, the heavier the system is and the more difficult it is to fold and stow
More »Organizations Performing Work | Role | Type | Location |
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Ames Research Center (ARC) | Lead Organization | NASA Center | Moffett Field, California |