Capstone Senior Design                      Idaho RISE                   NASA Idaho Space Grant Consortium

Home
Human Resources
Archive
Project Scoping
Project Definition
Design Development
Fabrication
Testing
Lessons Learned

 

 

Conceptual Design

bulletLiterature Review
bulletMechanical Design Concepts  
bulletMethod of Ascent
bulletProbe Shape
bulletMaterials
bulletRelease Mechanisms
bulletParachute Deployment
bulletParachute Design
bulletSensor Rods
bulletMechanical Decision Tables
bulletElectrical Design Concepts
bulletDesign Concepts
bulletElectrical Decision Tables
bulletProbe Prototypes

 

 

 

 

Mechanical Design Concepts

Sensor Rods:

We considered several concepts for the geometry of the sensor rod arms.  The main objective of these arms is to allow sensors to reach outside the boundary layer of the probe as it falls.  This allows the sensors to measure "un-disturbed" air and yields more accurate results.  One of our concerns in the sensor rod design was the structural stability of the rods during impact with the ground.  Because of this concern, the static cross design appears to be the best because it allows the possibility of multiple rods distributing the landing force.

Static Rods (linear design-one on either side 180˚ apart)

 

Static Rods (cross design-four rods 90˚ apart)

note: a sphere design is used here as an example shape.

 

Dynamic Rods

Designed for the aero-shell.   Rods deploy after the aero-shell detaches from the probe. 

 

 

Home | Human Resources | Archive | Project Scoping | Project Definition | Design Development | Fabrication | Testing | Lessons Learned

For problems or questions regarding this web contact [cyklein@uidaho.edu].
Last updated: 05/10/06.