Linear Actuator System for the NASA Docking SystemThe Linear Actuator System (LAS) is a major sub-system within the NASA Docking System (NDS). The NDS Block 1 will be used on the Boeing Crew Space Transportation (CST-100) system to achieve docking with the International Space Station. Critical functions in the Soft Capture aspect of docking are performed by the LAS, which implements the Soft Impact Mating and Attenuation Concept (SIMAC). This paper describes the general function of the LAS, the system's key requirements and technical challenges, and the development and qualification approach for the system.
Document ID
20170000501
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Dick, Brandon (Boeing Co. Houston, TX, United States)
Oesch, Chris (Moog, Inc. East Aurora, NY, United States)
Date Acquired
January 19, 2017
Publication Date
September 20, 2017
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-38403
Meeting Information
Meeting: European Space Mechanism and Tribology Symposium