The objective of ADEPT is to develop a semi-rigid low-ballistic coefficient aeroshell entry system concept to perform and entry descent landing (EDL) functions for planetary missions.
For the ADEPT deployable concept, woven carbon fabric (which covers 90% of the deployed surface and is supported by semi-rigid ribs) is the primary drag-producing surface. Its flexibility also allows it to be stowable. The pure carbon fabric, with its high thermal conductivity, allows re-radiation from both the windward and leeward side of the fabric. This activity will include the detailed design and fabrication of a sub-scale prototype test article (approximately 2-m diameter) that will include as many flight-like and mission-traceable aspects as possible. The ADEPT proto-flight configuration will undergo integrated ground testing including numerous deployments, random vibration and acoustic testing and thermal-vac. Planning for the execution of follow-on flight-testing is on-going.
Adaptable Deployable Entry Placement Technology (ADEPT)
To put footprints on Mars and deliver robotic payloads for breakthrough science investigations to Venus and beyond, spacecraft with larger deployable drag surfaces than can be launched on today’s rockets are needed.
One way to address this challenge is to launch a spacecraft that can be stowed and packed to fit onto currently available rockets and then be opened like an umbrella in space to provide the thermal protection system (TPS) and structural geometry needed to safely deliver human and robotic payloads to the planet surface.
ADEPT is a semi-rigid umbrella-like mechanical systemof ribs and struts covered with a specialized carbon cloth that provides both a TPS and a structural surface for drag. The advanced construction of the carbon fabric allows the vehicle skin to withstand the pressure load and very high temperatures encountered during the deceleration phase of planetary entry.