*HTML is ON
*UBB Code is ON
[i]"The nozzle impact during stage separation occurred due to a much higher than expected vehicle rotation rate of about 2.5 deg/sec vs. the maximum expected of 0.5 deg/sec. As the 2nd stage nozzle exited the interstage, the first stage was rotating so fast that it smacked the niobium nozzle," Musk noted. "There was no apparent damage to the nozzle, which is not a big surprise given that niobium is tough stuff.
"The unexpectedly high rotation rate was due to not knowing the shutdown transient of the 1st stage engine (Merlin) under flight conditions. The actual shutdown transient had a very high pitch over force, causing five times the max expected rotation rate."[/i]
If you have previously registered, but forgotten your password, click here.
*** Click here to review this topic. ***
Contact Us | The Source for Space History & Artifacts
Copyright 2017 collectSPACE.com All rights reserved.