INSTRON Testing - Bending from Drag/Lift, Shear Force
Objectives
Understand how defects in previous fin cans impact overall strength
Reference for making a 6” fin can for future spaceshot rocket
Future comparison to aluminum fin can
Heuristic Moment Comparisons
Hermes III | Phoenix | |
Max. Q | 9160 lb/ft^2 | 2735 lb/ft^2 |
Fin Area | 0.392 ft^2 | 0.128 ft^2 |
Product | 3588 lb | 349 lb |
Risks
Unfamiliarity with derivation and analysis
get trained! Go over procedure before actual testing to avoid having to test over and over again
Compatibility of INSTRON with setup
Communicate with Pierce to make necessary modifications
Bending Jig
INSTRON applies load on the faces of the fins that mimics moments from drag and lift
Fin can unconstrained around mandrel
Testing Procedure
Test in 10% load increments through proof load
Observe deformation throughout
Stress strain curve
Video
Fin itself bending or twisting
Calculate distance from fillet to bend fixture
Make sure bend fixture spans the length of the fin
Uneven application of loads
Account for jig, differences in manufacturing, testing 2 fins at once
Observe and take video to see if anything else deforms
Drag Jig
INSTRON clevis attaches to leading edge and pushes down to mimic shear from drag
Fin can unconstrained around mandrel
Testing Procedure
Test in 10% load increments through proof load
Observe deformation throughout
Stress strain curve
Video
Load not well distributed / twisting / slipping
Revise jig edge / clevis setup
Observe and take video to see if anything else deforms
Off-axis → base plate taking load
Can’t test to failure
Proof load small tests
Create bigger design to center the fin can and press on all 4 fins