Mission requirements
Define the functional, environmental, mechanical, and operational requirements of the CanSat system.
IN-SPACe National CANSAT Competition
Student spacecraft systems engineering, integration, and field testing carried out from 2022 to 2024.
Overview
This project involved the design and integration of a compact CanSat platform for the IN-SPACe National CANSAT Competition. The work included subsystem coordination, avionics integration, mechanical packaging, testing, and preparation for the national finals in Ahmedabad in April 2024.
This page is a developing technical record of the project. Architecture details, test data, and original photographs will be incorporated as they become available.
Project Objectives
Subsystem development
Integrate avionics, communications, power, structure, and recovery subsystems into a compact platform.
Verification and testing
Establish a sequence of subsystem checks, integration tests, and mission-readiness assessments.
Field operations
Prepare procedures for deployment, telemetry monitoring, retrieval, and post-test evaluation.
System Architecture
The sections below provide a general structure for the technical description. Specific components and performance figures will be added once verified.
Avionics and onboard software
Flight computer, sensor interfaces, data acquisition, state management, and software integration.
Telemetry and communications
Communication architecture, ground-side reception, telemetry packets, and operational monitoring.
Mechanical configuration
Packaging constraints, subsystem mounting, access for assembly, and structural integration.
Recovery and operations
Recovery-system interfaces, deployment considerations, safety checks, and field procedures.
Development and Validation
Design and prototyping
Initial system configuration, subsystem-level prototypes, interface definition, and iterative integration.
Integration and testing
Functional checks, hardware–software integration, telemetry verification, and preparation for field trials.
Project Gallery
A featured-image layout with supporting technical images. The placeholders below indicate where original project media can be added.
Featured project photograph
System architecture
Avionics and integration
Testing and operations
Results and telemetry
Gallery concept: one large hero image, followed by technical supporting images. All imagery is intentionally left as labeled placeholders.
Outcomes and Lessons Learned
The project culminated in participation in the national finals in Ahmedabad in April 2024. Detailed results, measured performance, engineering challenges, and lessons learned will be documented here after review of the project records.
Technical Resources
Project documentation, photographs, system diagrams, and supporting references will be linked here when prepared for publication.