The ADEPT architecture represents a completely new approach for entry vehicle design using a high-performance carbon fabric to serve as the primary drag surface of the mechanically deployed decelerator and to protect the payload from hypersonic aerothermal heating during entry. The initial system-level development of the nano-ADEPT architecture will culminate in the launch of a 0.7-m deployed diameter ADEPT sounding rocket flight experiment. The SR-1 sounding rocket flight experiment is a critical milestone in the technology maturation plan for ADEPT and will generate performance data on in-space deployment and aerodynamic stability
The Nano Entry System for CubeSat-Class Payloads led to the development of the Nano-Adaptable Deploy...
This paper describes aerothermodynamic and thermal structural testing that demonstrate the viability...
Analysis completed since the test suggests that all test objectives were met This claim will be veri...
On September 12th 2018, a sounding rocket flight test was conducted on a mechanically-deployed atmos...
A sounding rocket flight test was conducted on a mechanically-deployed entry vehicle (DEV) known as ...
The SR-1 flight experiment will demonstrate most of the primary end-to-end mission stages including:...
ADEPT is an atmospheric entry architecture for missions to most planetary bodies with atmospheres: C...
The proposed presentation will give an overview of a mechanically deployable entry system concept de...
There is growing interest for utilizing Small Satellites beyond low Earth orbit. A number of seconda...
Deployable entry vehicles provide an enabling capability for large payloads at destinations across t...
The Adaptive Deployable Entry and Placement Technology (ADEPT), a mechanically deployable entry vehi...
We propose to develop a robust guidance and control system for the ADEPT (Adaptable Deployable Entry...
A computational study of the Adaptive Deployable Entry and Placement Technology (ADEPT) Sounding Roc...
There is growing interest for utilizing Small Satellites beyond low Earth orbit. A number of seconda...
Conceptual Neptune orbiter was designed for the purpose of assessing mission feasibilityBuilt off of...
The Nano Entry System for CubeSat-Class Payloads led to the development of the Nano-Adaptable Deploy...
This paper describes aerothermodynamic and thermal structural testing that demonstrate the viability...
Analysis completed since the test suggests that all test objectives were met This claim will be veri...
On September 12th 2018, a sounding rocket flight test was conducted on a mechanically-deployed atmos...
A sounding rocket flight test was conducted on a mechanically-deployed entry vehicle (DEV) known as ...
The SR-1 flight experiment will demonstrate most of the primary end-to-end mission stages including:...
ADEPT is an atmospheric entry architecture for missions to most planetary bodies with atmospheres: C...
The proposed presentation will give an overview of a mechanically deployable entry system concept de...
There is growing interest for utilizing Small Satellites beyond low Earth orbit. A number of seconda...
Deployable entry vehicles provide an enabling capability for large payloads at destinations across t...
The Adaptive Deployable Entry and Placement Technology (ADEPT), a mechanically deployable entry vehi...
We propose to develop a robust guidance and control system for the ADEPT (Adaptable Deployable Entry...
A computational study of the Adaptive Deployable Entry and Placement Technology (ADEPT) Sounding Roc...
There is growing interest for utilizing Small Satellites beyond low Earth orbit. A number of seconda...
Conceptual Neptune orbiter was designed for the purpose of assessing mission feasibilityBuilt off of...
The Nano Entry System for CubeSat-Class Payloads led to the development of the Nano-Adaptable Deploy...
This paper describes aerothermodynamic and thermal structural testing that demonstrate the viability...
Analysis completed since the test suggests that all test objectives were met This claim will be veri...