This paper describes the development and design of the Astrobee Free-Flyer propulsion nozzle assemblies. As will be illustrated in this paper, the Free-Flyer nozzles are thrust control devices used to propel the Astrobee Free-Flyer robot autonomously inside the International Space Station (ISS). The development process, design evolution, and prototyping methods, are described. Key design features are discussed in greater detail to highlight how a seemingly simple design can present surprisingly large challenges. Several lessons learned are given.
Astrobee Free-Flyer Nozzle Mechanism
The 45th Aerospace Mechanism Symposium ; 2020 ; Houston, TX, US
Conference paper
No indication
English
Astrobee Space Station Robotic Free Flyer
NTRS | 2016
|Astrobee: Space Station Robotic Free Flyer
NTIS | 2016
|Astrobee: Space Station Robotic Free Flyer
NTRS | 2016
|