NASA/JPL Component Shock Testing Machine Qualification Shock Test Philosophy for Reusable Launch Vehicle Components by Tom Irvine MPE = Maximum Predicted Environment Proposed Rule: Initial Qualification (one flight): 3 shocks per axis at MPE + 6 dB For each additional flight: 1 shock per axis… Read more
Launch Vehicle Static Fire Test Explosion Fault Tree
Slide Link Static fire tests are among the most critical — and most dangerous — milestones in a launch vehicle’s life. The vehicle is fully fueled, the engines are lit, and everything that can go wrong is present in one place at one time. This… Read more