Publication Date:
2018-06-06
Description:
Traditional fairing systems are designed to fully encapsulate and protect their payload from the harsh ascent environment including acoustic vibrations, aerodynamic forces and heating. The Orion fairing separation system performs this function and more by also sharing approximately half of the vehicle structural load during ascent. This load-share condition through launch and during jettison allows for a substantial increase in mass to orbit. A series of component-level development tests were completed to evaluate and characterize each component within Orion's unique fairing separation system. Two full-scale separation tests were performed to verify system-level functionality and provide verification data. This paper summarizes the fairing spring, Pyramidal Separation Mechanism and forward seal system component-level development tests, system-level separation tests, and lessons learned.
Keywords:
Spacecraft Design, Testing and Performance; Launch Vehicles and Launch Operations; Mechanical Engineering
Type:
The 42nd Aerospace Mechanism Symposium; 273-286; NASA/CP-2014-217519
Format:
application/pdf
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