DRAFT: This module has unpublished changes.

Testing Plan

The rocket prototype was tested to ensure that the performance of the rocket met the customer requirements and the design specifications. A failure of just one subsystem of the rocket could potentially destroy the entire prototype. This high risk nature of a high power rocket requires extensive and thorough testing so that there will be confidence of the rockets performance on launch day. The high level block diagram of the units/ subsystems under test with interfaces is shown below. A majority of testing will be centered on the recovery of the rocket. This function requires the most moving parts and occurs in multiple stages.

 

Tests required are:

 

  • Safety Features:
    • Check backup flight boards
  • Airframe:
    • Airframe Dry Fit
    • Electronics Bay Strength
    • Drop Test of airframe
  • Electrical Bay:
    • Data Collection of Sensors
    • Flight Event Triggers
    • Data Transmission
  • Recovery Bay:
    • Nose Cone Ejection
    • Drogue and Mains Parachute Deployment/ Opening
    • Mains Release Mechanism
  • Full System Test (Flight)

DRAFT: This module has unpublished changes.