This document addresses vibration, shock, and acoustic environments. Tailoring and updates were motivated by lessons learned on launch and space programs, and by the increase in scope and applicability necessary in longstanding baseline requirements with the realization of reusable systems and evolving vehicle and mission architectures. It is intended that this document expands the applicability of dynamic environments requirements to a broader range of industry systems and practice. The content in this document was drawn largely from LE-T-013 (2019), entitled Dynamic Environments Tailoring and Guidance to SMC-S-016 for Expendable and Reusable Launch Vehicles. Material drawn from this was reviewed for further content updates and to ensure applicability to space vehicles with additions or modifications made where necessary. The updates that were proposed are presented as a tailoring document comprising the limited updates to the baselined requirements, rather than as an update to the core document.
Dynamic Environments Tailoring and Updates to TR-RS-2014-00016/SMC-S-016 (2014), Test Requirements for Launch, Upper-Stage and Space Vehicles
2021
41 pages
Report
No indication
English
Acceptance tests , Corporations , Dynamic tests , Electronic equipment , Engineering , Failure mode and effect analysis , Frequency bands , Launch vehicles , Life tests , Procurement , Random vibration , Resonant frequency , Shock tests , Space systems , Spacecraft , Test and evaluation , Test equipment
Overview of Space Launch System Ascent Aerothermal Environments (AIAA 2014-1257)
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