Cube Satellite Deployer Using ISS Robotic Arm
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Solution Overview
Problem
The existing methods for deploying cube satellites in space are time-consuming and costly, requiring individuals or organizations to either design and launch their own satellites or pay others to do so, which is not economically or timely viable for short-term needs.
Innovation Solution
A cube satellite deployer system that adapts existing cube satellite launchers to be attached to a space arm assembly, such as the one used on the International Space Station, allowing for the launch of cube satellites into orbit at reduced costs and increased accessibility.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Productivity
If traditional methods are used to launch cube satellites, then the satellite can be deployed into orbit, but the process is time-consuming and costly
Solution Approach 1:
Cube satellites are pre-assembled and tested on Earth before launch, with launchers prepared in advance. The space arm assembly is pre-positioned on the ISS to receive and deploy satellites without requiring complex in-orbit assembly operations, thereby reducing deployment time.
Solution Approach 2:
A specialized launcher vehicle serves as an intermediary between the cube satellite and the ISS space arm assembly. This intermediary carrier facilitates the transfer and deployment process, enabling rapid deployment by pre-positioning the satellite on the launcher before ISS arrival.
2Productivity
If traditional satellite launch methods are used, then cubesatellites can be launched into orbit, but the cost is high and not economically viable
Solution Approach 1:
The space arm assembly on the ISS is designed to perform multiple functions including scientific experiments, satellite deployment, and cargo transport. By utilizing this multi-functional platform for cube satellite deployment, the cost is significantly reduced compared to dedicated launch vehicles.
Solution Approach 2:
The system leverages the ISS infrastructure and space arm assembly to provide launch services, allowing cube satellites to be deployed using existing resources rather than requiring separate dedicated launch systems, thereby reducing overall deployment costs.
3Adaptability or versatility
If custom satellite designs are created for each user, then specific mission requirements can be met, but development time and cost increase
Solution Approach 1:
The satellite system is divided into modular components: standardized cube satellite platforms and configurable launchers. Users can select from standardized satellite modules and customize only the necessary components for their specific mission, reducing development time while maintaining adaptability.
Solution Approach 2:
The system allows customization through parameter changes rather than redesign. Users can modify mission parameters such as satellite size, payload capacity, and orbital characteristics within standardized configurations, enabling mission-specific requirements to be met without extending development cycles.
Data Source
AI summary
A cube satellite deployer system having a body plate, a communication unit, a power unit, and a control unit. The body plate is adapted to be connected to a space arm assembly. The communication unit and the power unit are attached to the body plate. Each of the communication unit, power unit, and the control unit are in communication with one another. The body plate is also adapted to receive one or more cube satellite housings. The cube satellite housings are adapted to house and selectively launch one or more of the cube satellites that are housed by the cube satellite housings.