Publication Date:
2019-08-13
Description:
The NASA Engineering and Safety Center (NESC) and Lockheed Martin (LM) performed random vibration testing on a single spring strut development unit to assess its ability to withstand qualification level random vibration environments. Failure of the strut while exposed to random vibration resulted in a follow-on failure investigation, design changes, and additional development tests. This paper focuses on the results of the failure investigations referenced in detail in the NESC final report including identified lessons learned to aid in future design iterations of the spring strut and to help other mechanism developers avoid similar pitfalls.
Keywords:
Spacecraft Design, Testing and Performance
Type:
M14-3169
,
Aerospace Mechanisms Symposium; May 14, 2014 - May 16, 2014; Baltimore, MD; United States
Format:
application/pdf