The Deployable Retrievable Boom which was developed as a part of the joint U.S.-Italian Tethered Satellite System (TSS) is described. The design mission of the boom is to support, deploy, and retrieve an experiment package for the study of the electromagnetic field surrounding the satellite. The mechanism includes a jettisoning provision and deployable harness for the supported payloads connection. The boom is based on a tubular telescopic concept. Particular emphasis is placed on the payload harness connection capability and safety provisions
In the early 1990's US and Italian scientists collaborated to study the electrodynamics of dragging ...
One of the key challenges for small satellites is packaging and reliable deployment of structural bo...
The in-situ exploration of planetary surfaces by lander vehicles requires in most cases suited deplo...
A new deployable and retractable telescoping boom capable of high deployed stiffness and strength is...
A special telescopic boom has been design-optimized, developed and qualified to carry an S-band ante...
In any sounding rocket, volume and mass are at a premium. Payload designers strive towards smaller, ...
This thesis deals with the further development of a boom deployment mechanism with integrated boom r...
A larger, stronger deployable boom was developed to handle the requirements of larger, heavier paylo...
CLUSTER is a scientific space mission to in-situ investigate the Earth's plasma environment by means...
A yo-yo-type wire-boom deployment system has been developed and flight tested on a sounding rocket m...
A new tubular boom deployment mechanism has been designed, built, and flown as part of the second Wa...
In 2005, NASA commenced Phase 1 of the Modular Reconfigurable High Energy Technology Demonstrator (M...
An innovative Deployment and Retraction hinge Mechanism (DARM) in the frame of a technological progr...
Development and operation of metal ribbon which acts like self deploying boom are described. Metal r...
The number of space debris orbiting our Earth has been continuously increasing since the beginning o...
In the early 1990's US and Italian scientists collaborated to study the electrodynamics of dragging ...
One of the key challenges for small satellites is packaging and reliable deployment of structural bo...
The in-situ exploration of planetary surfaces by lander vehicles requires in most cases suited deplo...
A new deployable and retractable telescoping boom capable of high deployed stiffness and strength is...
A special telescopic boom has been design-optimized, developed and qualified to carry an S-band ante...
In any sounding rocket, volume and mass are at a premium. Payload designers strive towards smaller, ...
This thesis deals with the further development of a boom deployment mechanism with integrated boom r...
A larger, stronger deployable boom was developed to handle the requirements of larger, heavier paylo...
CLUSTER is a scientific space mission to in-situ investigate the Earth's plasma environment by means...
A yo-yo-type wire-boom deployment system has been developed and flight tested on a sounding rocket m...
A new tubular boom deployment mechanism has been designed, built, and flown as part of the second Wa...
In 2005, NASA commenced Phase 1 of the Modular Reconfigurable High Energy Technology Demonstrator (M...
An innovative Deployment and Retraction hinge Mechanism (DARM) in the frame of a technological progr...
Development and operation of metal ribbon which acts like self deploying boom are described. Metal r...
The number of space debris orbiting our Earth has been continuously increasing since the beginning o...
In the early 1990's US and Italian scientists collaborated to study the electrodynamics of dragging ...
One of the key challenges for small satellites is packaging and reliable deployment of structural bo...
The in-situ exploration of planetary surfaces by lander vehicles requires in most cases suited deplo...