At today, few mating technologies for nano and micro satellites have been designed and tested in relevant environment, despite the raising interest in making such platforms able to join, separate and independently reconfigure. In this framework, this paper presents a review of the research activities carried out in the last five years at the University of Padova with respect to small satellites docking mechanisms. Research in this field began with the projects ARCADE project (Autonomous Rendezvous, Control And Docking Experiment) and its re-flight ARCADE-R2, that made it possible to develop and test a small-scale gender-mate mechanism inspired by Soyuz and ATV docking systems. As a concurrent solution to the ARCADE probe-drogue configurati...
On-orbit operations such as refuelling, payload updating, inspection, maintenance, material and crew...
Docking small satellites in space is a high-risk operation due to the uncertainty in relative positi...
In-orbit docking technology of microsatellites to realize combined reconfiguration has a wide applic...
Since the first mating manoeuvre performed in 1966 between the Gemini VIII and the Agena Target Vehi...
Since the first mating manoeuvre in space, performed in 1966, many different docking mechanisms were...
The development of on-orbit autonomous rendezvous and docking (ARD) capabilities represents a key po...
Docking mechanisms have been employed in space missions for more than 50 years. In fact, since the A...
This paper presents the design and characterization of a miniature docking mechanism for nanosatelli...
This dissertation addresses the design procedure of a docking mechanism for space applications, in p...
This slide presentation reviews the different types of docking types. The objective is the pressuriz...
This paper provides an overview of the ARCADE-R2 experiment, which is a technology demonstrator that...
In recent years there has been a continuously growing interest in space missions conducted with mini...
The main topic of this work is the design of a docking mechanism for the STRONG mission. This forese...
The objective of the STRONG mission is the deployment of payloads from Low Earth Orbit into greater ...
This paper discloses the design procedure of a docking mechanism for space applications. The mechani...
On-orbit operations such as refuelling, payload updating, inspection, maintenance, material and crew...
Docking small satellites in space is a high-risk operation due to the uncertainty in relative positi...
In-orbit docking technology of microsatellites to realize combined reconfiguration has a wide applic...
Since the first mating manoeuvre performed in 1966 between the Gemini VIII and the Agena Target Vehi...
Since the first mating manoeuvre in space, performed in 1966, many different docking mechanisms were...
The development of on-orbit autonomous rendezvous and docking (ARD) capabilities represents a key po...
Docking mechanisms have been employed in space missions for more than 50 years. In fact, since the A...
This paper presents the design and characterization of a miniature docking mechanism for nanosatelli...
This dissertation addresses the design procedure of a docking mechanism for space applications, in p...
This slide presentation reviews the different types of docking types. The objective is the pressuriz...
This paper provides an overview of the ARCADE-R2 experiment, which is a technology demonstrator that...
In recent years there has been a continuously growing interest in space missions conducted with mini...
The main topic of this work is the design of a docking mechanism for the STRONG mission. This forese...
The objective of the STRONG mission is the deployment of payloads from Low Earth Orbit into greater ...
This paper discloses the design procedure of a docking mechanism for space applications. The mechani...
On-orbit operations such as refuelling, payload updating, inspection, maintenance, material and crew...
Docking small satellites in space is a high-risk operation due to the uncertainty in relative positi...
In-orbit docking technology of microsatellites to realize combined reconfiguration has a wide applic...