This was a successful test that used 0.2 grams of black powder in the piston and 3x 6-32 shear pins. Webbing was used to connect the sections and the rocket contained a drogue and main parachute. Webbing lengths were not representative but were merely a mock-up of the planned webbing lengths (excluding a load path for the tender descender, which was not included in this test). This test did not implement any form of flight avionics. Following the test, we also performed a tug-test on the parachute, the results of which are summarized below.
Test Case | Approximate Maximum Force (lbs) |
---|---|
Fish scale attached to drogue shroud-line quicklink; pulled main parachute out of cup. | 4.52 |
Held the top of the deployment bag in place; attached the fish-scale to the main parachute's shroud-line quicklink; pulled main chute out of deployment bag. | 9.02 |
Black Powder Calculations
This ground test used 0.2 grams of black powder, which was calculated in the following manner:
Step 1: Determine volume in the piston prior to rod extension
Step 2: Determine necessary force to break shear pins
Step 3: Determine PSI inside the piston necessary to achieve required force
360 lb-f = x * 0.5184π in2
x = 221 psi
Step 4: Determine PSI inside the piston necessary to achieve required force
Using this black powder calculator and the previous quantities, we determined that 0.2 grams of black powder would be necessary to achieve 360 lb-f.
Step : Evaluate Assumptions
- Admittedly this math is sensitive to the volume, which we only estimated.
- The BP calculator assumes an ideal gas, which isn't true.
Media
Video of test: Ground Test 12-2.MOV
During the previous ground test, the large amount of force applied (estimated at 3500 pounds), damaged the fin can coupler's bolt holes, pushing the coupler further into the fin can. This made mating the fin can with the mission package difficult during integration.
Image of the rocket after separation.
Close-up of the rocket after the ground test.
The black powder did not travel very far up the bore of the piston.